Aircraft Report for n917wn



Registration History for n917wn






N-Number Make Model Serial Location Description Time
N917WN BOEING 737-7H4 36624 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2008-04-01, expiration date 2023-06-30, serial number 36624. 2020-02-04
N917WN BOEING 737-7H4 36624 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2008-04-01, expiration date 2020-06-30, serial number 36624. 2017-02-07
N917WN BOEING 737-7H4 36624 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2008-04-01, expiration date 2017-06-30, serial number 36624. 2014-02-24
N917WN BOEING 737-7H4 36624 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2008-04-01, expiration date 2017-06-30, serial number 36624. 2014-02-24
N917WN BOEING 737-7H4 36624 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2008-04-01, expiration date 2014-06-30, serial number 36624. 2011-06-18

Service Difficulty Reports for n917wn















































































































































































































N-Number Make Model Serial Description Time
N917WN BOEING 7377H4 During INSP/MAINT - FWD ENTRY DOOR EMERGENCY HANDLE LOOSE / [01] TIGHTENDED FWD ENTRY DOOR EMERGENCY HANDLE PER AMM 25-21-31-420-802 STEP 3B(6);[02] VERIFIED CORRECTIVE ACTION #1 2022-10-18
N917WN BOEING 7377H4 During INSP/MAINT - AFT GALLEY POWER SUPPLY (BATTERY) M1673 INOP. AFT EMERGENCY EXIT LIGHTS NOT WORKING / [01] R&R AFT GALLEY EMERGENCY LIGHT BATTERY PACK REF AMM 33-51-06<BR>OPS CHECK GOOD. 2022-06-08
N917WN BOEING 7377H4 During INSP/MAINT - CABIN AREA FLOOR SUPPORT ANGLE 312 TO 328 LBL 45 CRACKED AT UPPER SURFACE / REMOVED & REPLACED FLOOR SUPPROT ANGLE BETWEEN STA ; 312 THRU STA 328 AND LBL 45 AS PER BOEING DRAW . # 141A5400 AND B737-7 SRM 51-40-02-0G-0 . 2022-05-25
N917WN BOEING 7377H4 During INSP/MAINT - SUPPLEMENTAL INFORMATION: ELEVATOR HINGE PANEL 344GB HAS A CRACK ON UNDERSIDE / REPAIRED AT ELEVATOR PANEL 344GB PER B737-700 SRM 51-70-06-2R-6. MATERIAL USED P.O 1150381; P.O 1624260 AND P.O 1614988 2022-05-25
N917WN BOEING 7377H4 During INSP/MAINT - CRACK ON ANGLE AT AFT CARGO COMPARTMENT FWD BULKHEAD STA 727 AND BL-0 [MARKED WITH RED DOT] / REMOVED AND REPLACED AFT CARGO COMPT FWD BULKHEAD STA 727 AND BL-0 BRACKET PER B737-700 SRM 51-40-02-0G-0 AND B DWG 144A9401 2022-05-25
N917WN BOEING 7377H4 During INSP/MAINT - SUPPLEMENTAL INFORMATION: FOUND CRACK AT FRAME STRUCTURE STA 312 AT L1 DOOR UPPER SILL BETWEEN STRINGER 5L AND STRINGER6L . / PERFORMED HFEC AT L1 DOOR UPPER SILL BETWEEN STR 5L AND STR 6L VERIFIED CRACK. TRIMMED OUT FRAME AND REMOVED DAMAGE. PERFORMED HFEC ON TRIM OUT; NO CRACKS FOUND. PERFORMED HFEC ROTO ON OPEN HOLES; NO CRACKS FOUND. FABRICATED AND HEATTREATED REPAIR ANGLE. TREATED AND PRIMED REPAIR ANGLE AND REPAIR AREA. INSTALLED REPAIR ANGLE IN REF B737 SRM 51-40-02-0G-0; AAR RES #2015426-2 REV IR AND SWA EA #1-753-36114 REV IR 2022-05-25
N917WN BOEING 7377H4 During INSP/MAINT - FWD CABIN FLOOR SUPPORT INTERCOSTAL CRACKS BETWEEN STA 380 & 400 AT RBL 10 MKD / REMOVED AND INSTALLED NEW FLOOR SUPPORTINTERCOSTAL BETWEEN STA 380 TO 400 RBL 10' AT FWD CABIN IAW B737 SRM 51-40-02-0G-0 2022-05-25
N917WN BOEING 7377H4 During INSP/MAINT - LEFT WING FLAP SUPPORT FAIRING PANEL#542AB; SEAL SUPPORT BRACKET IS CRACK; OUTBOARD SIDE; FOWARD. DOT# 005 / REMOVED ANDREPLACED CRACKED SEAL SUPPORT BRACELET AT LEFTFLAP SUPPORT FAIRING PANEL #542 AB IN REF WITH B737-700 SWA SRM 51-40-02-0G-0 2022-05-24
N917WN BOEING 737 During INSP/MAINT - SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; RIGHT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727E+15. ; / [01] INSPECTED.; [02] REMOVED AND REPLACED AFT CARGO R/H TRANSITION FROM STA. 727 TO STA. 767 PER SRM 51-40-02 2022-05-09
N917WN BOEING 737 During INSP/MAINT - SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE AT STA.727C+2; / [01] REMOVED AND REPLACED AFT CARGO R/H TRANSITION ANGLE FROM STA. 727 TO STA 767 PER SRM 51-40-02; [02] INSPECTED. 2022-05-09
N917WN BOEING 737 During INSP/MAINT - SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727B+10. ; / [01]UPDATED PARTS INFORMATION.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-10-02.; [03] R&R?D L/HTRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [04] INSPECTED.; [05] CORRECTED CORROSION QUESTIONS 2022-05-09
N917WN BOEING 737 During INSP/MAINT - SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; RIGHT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.767+5. ; / [01]REMOVED END REPLACED TRANSITION ANGLE STA 767 TO 794.3 PER SRM 51-40-02. 2022-05-09
N917WN BOEING 737 During INSP/MAINT - SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727C+10. ; / [01]R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [02] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASEADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-05-09
N917WN BOEING 737 During INSP/MAINT - SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727D+14. ; / [01]R&R?D L/H TRANSITION ANGLE IAW SRM 51-40-02.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-05-09
N917WN BOEING 737 During INSP/MAINT - SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+9. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED .005?. ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLEFROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-05-09
N917WN BOEING 737 During INSP/MAINT - SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; RIGHT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.767+14. ; / [01]UPDATED CORROSION QUESTIONS; [02] REMOVED DAMAGE PER SRM 53-60-15-1A-1 AND FOUND TO BE OUT-OF-LIMITS PER SRM 53-60-15-1A-1.; [03] LOCATED; DRILLED AND DEBURRED REPLACEMENT SHIELD PER SRM 51-40-05.; [04] REMOVED DAMAGE PER SRM 53-60-15-1A-1AND FOUND TO BE OUT-OF-LIMITS PER SRM 53-60-15-1A-1. LOCATED; DRILLED AND DEBURRED REPLACEMENT SHIELD PER SRM 51-40-05.INSPECTION C/W ON CA #2 AND #3.; [05] REMOVED AND REPLACED FWD SHIELD; STA 767 TO STA 794.3 PER SRM 51-40-02. 2022-05-09
N917WN BOEING 737 During INSP/MAINT - SUPPLEMENTAL INFORMATION: AFT CARGO COMPARTMENT; RIGHT TRANSITION CORROSION AROUND FASTENER HOLE FROM STA.747 TO STA.767. ; / [01] REMOVED AND REPLACE AFT CARGO R/H TRANSITION ANGLE FROM STA. 727 TO STA. 767 PER SRM 51-40-02; [02] INSPECTED. 2022-05-09
N917WN BOEING 737 During INSP/MAINT - SUPPLEMENTAL INFORMATION: ATTACH BRACKET HAS ELONGATED HOLE FOR AFT CARGO DOOR CUTOUT FWD SHIELD AT STA 767. ; / [01] REMOVED AND REPLACED ATTACH BRACKET IAW SRM 51-40-02. 2022-05-09
N917WN BOEING 737 During INSP/MAINT - SUPPLEMENTAL INFORMATION: AFT GALLEY DOOR SLIDE SAFETY PIN NOT STOWED (INSIDE THE SLIDE COVER) ; / [01] STOWED AFT GALLEY DOOR SLIDE SAFETY PIN PER AMM 25-66-01.; [02] VERIFIED SELECT REFERENCE ADDED 2022-05-09
N917WN BOEING 737 During INSP/MAINT - SUPPLEMENTAL INFORMATION: AFT CARGO THRESHOLD WEB HAS SURFACE CORROSION AROUND FASTENER HOLES. MARKED ; / [01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [02] INSPECTION C/W ON CA #1.; [03] PARTS DATA UPDATE ONLY; [04] LOCATED AND DRILLED NEW THRESHOLD WEB PER SRM 51-40-05.; [05] AFT CARGO THRESHOLD WEB REMOVEDFOR REPLACEMENT PER SRM 51-40-02; [06] VERIFIED LOCATED AND DRILLED; [07] INSTALLED NEW WEB PER SRM 51-40-02 2022-05-09
N917WN BOEING 7377H4 During UNKNOWN - SUPPLEMENTAL INFORMATION: RT. WING EMERGENCY EXIT DOOR OVERHEAD LIGHT COVER IS LOOSE. / CLOSING ACTION LOG# 0161814 R&REXIT SIGN LIGHT ASSEMBLY IAW AMM 33-51-01. OPS CHECK SATIS NO OTHER DEFECTS NOTED. CLEARING# 39594 2022-05-04
N917WN BOEING 7377H4 During INSP/MAINT - FWD MAIN CABIN FLOOR PANEL 221BF CORNER CRACKED / RECEIVED NEW FLOOR PANEL 221BF; PANEL INSTALLATION WILL BE ACCOMPLISHED ON WORK CARD (JPANEL-221-CLOSE) 2022-04-15
N917WN BOEING 7377H4 During NOT REPORTED - AFT CARGO COMP SCUFF PLATE FWD CORNER FOUND CRACK / RECEIVED NEW PART (P# 7530063) SCUFF PLATE FWD CORNER THIS SCUFF PLATE FWD CORNER WILL BE INSTALL ON J-753-721-00-01 2022-04-04
N917WN BOEING 7377H4 During NOT REPORTED - L-1 DOOR FWD I/B SCUFF PLATE FOUND CRACK AT FASTNER HOLE / RECEIVED NEW SCUFF PLATE FOR L-1 DOOR FWD I/B SECTION PART#7252178. SCUFF PLATE WILL BE INSTALLED JOB CARD:J725-025-00-01Y(2015423/2000/0007) 2022-04-04
N917WN BOEING 7377H4 During INSP/MAINT - FAIRING 193B HAS NUMEROUS ELONGATED HOLES / REMOVED AND REPLACED 193B FAIRING PER AMM 53-51-21 2022-03-24
N917WN BOEING 7377H4 During INSP/MAINT - FWD CARGO - INTERCOSTAL CRACKED BETWEEN STA 500A - 500B; LBL 24. / REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02. 2022-03-09
N917WN BOEING 7377H4 During INSP/MAINT - RUDDER BALANCE WEIGHT CORRODED L/H O/B SIDE. / REMOVED AND REPLACED RUDDER BALANCE WEIGT PER SRM 51-60-07-0G-0 PARAGRAPH(11) STEP (C) TO D).CORROSION AND ATA QUESTIONS ANSWERED. 2022-03-04
N917WN BOEING 7377H4 During INSP/MAINT - WHILE PERFORMING DAMAGE CUTOUT INSPECTION; FOUND TOOLING DAMAGE ON COCKPIT FLOOR MOUNT CHANNEL ALONG L/H EDGE OF DAMAGECUTOUT. / REPAIRED COCKPIT FLOOR MOUNT CHANNEL IAW EA 1-753-31995 PART 2. 2022-03-04
N917WN BOEING 7377H4 During INSP/MAINT - AFT. CARGO COMPARTMENT CORROSION ON L/H TRANSITION ANGLE AROUND FLOOR PANEL FASTENER HOLE AT STA. 747+9. / L/H TRANSITION ANGLE REMOVED AND REPLACED FROM STA. 747+8 TO 807+11; ALL WORK ACCOMPLISHED ON G509781 2022-03-04
N917WN BOEING 7377H4 During INSP/MAINT - AFT. CARGO COMPARTMENT CORROSION ON L/H TRANSITION ANGLE AROUND FLOOR PANEL FASTENER HOLES IN BETWEEN STA. 767+3 AND STA. 807+10.5 / REMOVED AND REPLACED L/H TRANSITION ANGLE SECTION STA. 755-817 PER SRM 53-00-53-2R-5. SEE WIP'S AND TASK'SFOR INDIVIDUAL SIGN OFFS. 2022-03-04
N917WN BOEING During UNKNOWN - FWD SERVICE DOOR ; BEAM #4 HAS CRACK INDICATION IN RADIUS AT INBOARD HOLE ; / [01] INFO: PLEASE HAVE INSPECTION BUYOFF FAULT TTG8Q00A4NDR WHEN THIS DOOR IS REPLACED.; [02] REMOVED AND REPLACED R1 DOOR GUIDE ARM AND ROLLER PER AMM 52-41-21.;[03] REMOVED AND REPLACED R1 DOOR UPPER TORQUE TUBE LINK ASSEMBLY PER AMM 52-41-41.; [04] INSPECTED WORK PERFORMED IN C/A #2 & #3; [05] REMOVED AND REPLACED R1 DOOR PER AMM 52-41-00.; [06] RIGGED R1 DOOR PER AMM 52-41-00.; [07] APPLIED CICTO R1 DOOR PER AMM 51-00-59.; [08] INSPECTED WORK PERFORMED IN C/A #7; [09] RIGGED FWD SERVICE DOOR (R-1) PER AMM 52-41-00.; [10] C/W; [11] C/W; [12] ALL INSPECTION WORK COMPLIED WITH. SEE INDIVIDUAL SIGN OFFS FOR ALL WORK PERFORMED.; [13] 2022-03-02
N917WN BOEING During UNKNOWN - FWD CARGO AFT R/H BULKHEAD LOWER CURVED 'L' ANGLE AT STA 500D HAS CORROSION LOWER END. (MARKED) ; / [01] FOUND TO BE OUTOF LIMITS PER SRM 53-30-08-1A-1.; [02] 1. DANIEL ANDERSON (TECHNICIAN); 11-JAN-2022 05:56 UTC<BR>FOUND TO BE OUT OF LIMITS PER SRM 53-30-08-1A-1. INSPECTED.; [03] LOCATED AND DRILL NEW R/H BULKHEAD ANGLE PER SRM 51-40-05.; [04] 3. DANIEL ANDERSON (TECHNICIAN); 11-JAN-2022 08:48 UTC<BR>LOCATED AND DRILL NEW R/H BULKHEAD ANGLE PER SRM 51-40-05. INSPECTED. 2022-03-02
N917WN BOEING During UNKNOWN - LT WING I/B UPPER WING ROOT PANEL SUPPORT CLIP CRACKED ABOVE TANK 1 BOOST PUMP ; / [01] R/R SUPPORT CLIP PER SRM 51-40-02 2022-03-02
N917WN BOEING During UNKNOWN - FWD CARGO R/H TRANSITION ANGLE HAS CORROSION AROUND NUMEROUS FASTENER HOLES BETWEEN STA 500A THRU 500D. (MARKED). ; / [01] REMOVED FWD CARGO RH TRANS ANGLE FROM STA 500A TO 500D.; [02] OUT OF LIMITS PER SRM 53-00-53-1A-2.; [03] LOCATED ANDBACK DRILLED HOLES IN NEW RH TRANSITION ANGLE FROM STA 500A TO 500D PER SRM 51-40-05-0G-0.; [04] C/W INSPECTION STEPS 1-3; [05] ALODINED AND PRIMED RH TRANSITION ANGLE FROM STA 500A TO STA 500D PER SOPM 20-41-02.; [06] INSPECTED ALODINED AND PRIMED LH TRANSITION ANGLE FROM STA 396 TO STA 500D PER SOPM 20-41-02.; [07] INSTALLED NUTPLATES ON RH TRANSITION ANGLE FROM STA 500A TO 500D PER 51-40-10-2R-0.; [08] VERIFIED STEPS 5;6 AND 7.; [09] APPLIED PAINT TO RH TRANS ANGLE FROM ST 2022-03-02
N917WN BOEING During UNKNOWN - FWD CARGO TRANSITION ANGLE JUST AFT OF DOOR CUTOUT R/H HAS CORROSION ON NUMEROUS FASTENER HOLES BETWEEN STA 480+15 THRUSTA 500A. (MARKED) ; / [01] LOCATED AND DRILLED NEW TRANSITION ANGLE IAW SRM 53-40-01.; [02] LOCATED AND DRILLED NEW TRANSITION ANGLE IAW SRM 53-40-01. ANGLE ENAMELED AND INSTALLED ON ROUTINE CARD TTG8Q004G007.; [03] LOCATED AND DRILLED NEWTRANSITION ANGLE IAW SRM 51-40-02. ANGLE ENAMELED AND INSTALLED ON ROUTINE CARD TTG8Q004G007. 2022-03-02
N917WN BOEING During UNKNOWN - FWD CARGO STA 500D LOWER BULKHEAD 'L' ANGLE HAS CORROSION AROUND RBL 17 THRU RBL 22. (MARKED) ; / [01] REMOVED CORROSIONFOUND TO BE OUT OF LIMITS; INSTALL OF NEW P/N 143A9485Y35 WILL BE ACCOMPLISHED ON TTG8Q004G007 STEP 42 PER SRM 53-00-53AND 5330-E-16461-NG; [02] 1. MICHAEL STANLEY (TECHNICIAN); 11-JAN-2022 15:53 UTC<BR>REMOVED CORROSION FOUND TO BE OUT OF LIMITS; INSTALL OF NEW P/N 143A9485Y35 WILL BE ACCOMPLISHED ON TTG8Q004G007 STEP 42 PER SRM 53-00-53 AND 5330-E-16461-NG INSPECTED.; [03] REMOVED AND REPLACEMENT OF PART WILL BE ACCOMPLISHED ON TTG8Q004G007 STEP 42. 2022-03-02
N917WN BOEING During UNKNOWN - FWD CARGO L/H TRANSITION ANGLE HAS CORROSION AROUND NUMEROUS FASTENER HOLES BETWEEN STA 500+14 THRU STA 500C+8 (MARKED).; / [01] OUT OF LIMITS PER SRM 53-00-53-1A-2.; [02] REMOVED FWD CARGO LH TRANS ANGLE FROM STA 396 TO 500D.; [03] LOCATED AND BACK DRILLED HOLES IN NEW LH TRANSITION ANGLE FROM STA 488 TO 500D PER SRM 51-40-05-0G-0.; [04] C/W INSPECTION OFSTEPS 1;2;AND 3; [05] ALODINED AND PRIMED LH TRANSITION ANGLE FROM STA 396 TO STA 500D PER SOPM 20-41-02.; [06] INSPECTED ALODINED AND PRIMED LH TRANSITION ANGLE FROM STA 396 TO STA 500D PER SOPM 20-41-02.; [07] INSTALLED NUTPLATES ON LH TRANSITION ANGLE FROM STA 488 TO 500D PER SRM 51-40-10-2R-0.; [08] VERIFIED STEPS 5;6AND 7.; [09] APPLIED PAINT TO LH TRAN 2022-03-02
N917WN BOEING During UNKNOWN - FWD CARGO SMALL TRANSITION ANGLE JUST FWD OF DOOR CUTOUT IS DEFORMED AFT END.(MARKED) ; / [01] LOCATED AND DRILLED NEW TRANSITION ANGLE PER SRM 53-40-01; [02] LOCATED AND DRILLED NEW TRANSITION ANGLE PER SRM 53-40-01.<BR>INSPECTION C/W.; [03] INSTALLED PER SRM 51-40-02; [04] INSTALLED PER SRM 51-40-02. INSPECTION C/W. 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE AT STA.727B+6 ; / [01] LINE 13 IN MEASUREMENTS IS INCORRECTLY NA. IT SHOULD READ 155.5; [02] REMOVED AND REPLACED AFT CARGO R/H TRANSITION ANGLE FROM STA. 727TO STA 767; [03] REMOVED AND REPLACED AFT CARGO R/H TRANSITION ANGLE FROM STA. 727 TO STA 767 PER SRM 51-40-02; [04] INSPECTED. 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727C+6. ; / [01] R&R?D L/H TRANSITION ANGLEFROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [02] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727C+14. ; / [01] R&R?D L/H TRANSITION ANGLE IAW SRM 51-40-02.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE FROM STA.747 TO STA.767. ; / [01] CORROSION FOUNDTO BE OUT OF LIMITS; REMOVED .006? .ALL WORK DONE IAW SRM 53-00-53-1A-2.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINALW (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE FROM STA.727E TO STA.747. ; / [01] CORROSION FOUNDTO BE OUT OF LIMITS. ALL WORK DONE IAW SRM 53-00-53-1A-2.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATERLINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727D+7. ; / [01] REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE IAW SRM 51-40-02.; [03] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [04] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADDFOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.767+3. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED .007? ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATERLINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+2. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS;M REMOVED .OO5? ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+9. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED .005?. ALL WORK DONE IAW SRM 53-00-53-1A-1.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+14. ; / [01] CORROSION FOUND TO BE OUTOF LIMITS. REMOVED .008? ALL WORK DONE IAW SRM 53-00-53-1A-1.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.767+7. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED .009?; ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847IAW SRM 51-40-02.; [03] INSPECTED.<BR>PLEASE ADD MEASUREMENT 13. WATER LINE. 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE AT STA.727C+2 ; / [01] REMOVED AND REPLACED AFT CARGO R/H TRANSITION ANGLE FROM STA. 727 TO STA 767 PER SRM 51-40-02; [02] INSPECTED. 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+11. ; / [01] CORROSION FOUND TO BE OUTOF LIMITS. REMOVED .006?. ALL WORK DOWN IAW SRM 53-00-53-1A-2.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE FROM STA.727D TO 727E' ; / [01] REMOVEDAND REPLACED AFT CARGO RIGHT TRANSITION ANGLE FROM STA. 727 TO STA. 767 PER SRM 51-40-02; [02] INSPECTED. 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; RIGHT TRANSITION CORROSION AROUND FASTENER HOLE FROM STA.747 TO STA.767. ; / [01] REMOVED AND REPLACE AFT CARGO R/H TRANSITION ANGLE FROM STA. 727 TO STA. 767 PER SRM 51-40-02; [02] INSPECTED. 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; RIGHT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727E+15. ; / [01] INSPECTED.; [02] REMOVEDAND REPLACED AFT CARGO R/H TRANSITION FROM STA. 727 TO STA. 767 PER SRM 51-40-02 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727B+10. ; / [01] UPDATED PARTS INFORMATION.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-10-02.; [03] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [04] INSPECTED.; [05] CORRECTED CORROSION QUESTIONS 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; RIGHT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.767+5. ; / [01] REMOVED END REPLACED TRANSITION ANGLE STA 767 TO 794.3 PER SRM 51-40-02. 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727C+10. ; / [01] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [02] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727D+14. ; / [01] R&R?D L/H TRANSITION ANGLE IAW SRM 51-40-02.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; RIGHT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.767+14. ; / [01] UPDATED CORROSION QUESTIONS; [02] REMOVED DAMAGE PER SRM 53-60-15-1A-1 AND FOUND TO BE OUT-OF-LIMITS PER SRM 53-60-15-1A-1.; [03] LOCATED; DRILLED AND DEBURRED REPLACEMENT SHIELD PER SRM 51-40-05.; [04] REMOVED DAMAGE PER SRM 53-60-15-1A-1 AND FOUND TO BE OUT-OF-LIMITS PER SRM 53-60-15-1A-1. LOCATED; DRILLED AND DEBURRED REPLACEMENT SHIELD PER SRM 51-40-05. INSPECTION C/W ON CA #2 AND #3.; [05] REMOVED AND REPLACED FWD SHIELD; STA 767 TO STA 794.3 PER SRM 51-40-02. 2022-03-02
N917WN BOEING During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+9. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED .005?. ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - WIGGLE PLATE ON RIGHT WING AT STATION ORSS 375 + 27 PHENOLIC STRIPE CRACKED IPC 57-50-00-20 ITEM 253 ; / [01] REMOVED AND REPLACED WIGGLE PLATE ON RIGHT WING AT STATION ORSS 375 + 27 PER SRM 51-40-02; [02] C/W 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - VARIOUS BULLNOSE EMERGENCY LIGHTS ARE OUT. ; / [01] REPLACED FWD L/H CIELING EMERG. BATTERY PACK AND CHARGING UNIT PER MM 33-51-06 OPS CHECKS GOOD.; [02] C/W INSPECTION 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - FWD CARGO FWD CORNER SCUFF PLATE CRACKED ; / [01] LOCATED AND DRILLED FWD CORNER SCUFF PLATE PER SRM 51-40-02; [02] INSPC/W TASK CARD CORRECTIVE ACTION #1.; [03] CORNER SCUFF PLATE TO BE INSTALLED ON TTG8Q002ELJ2 AND LEAK CHECK ON TTG8Q00A0DA3; [04] VERIFIED C/A #3 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT THRESHOLD ACT CORNER SCUFF PLATE IS CRACKED ; AFT CARGO COMPARTMENT THRESHOLD AFT CORNER SCFF PLATE IS CRACKEDACT IS A TYPO AND SHOLD SAY AFT / [01] AFT CARGO COMPARTMENT REMOVED AND REPLACED THRESHOLD AFT CORNER SCUFFPLATE PER AMM 53-11-02-401; [02] PRESSURIZATION LEAK CHECK WILL BE PERFORMED ON TASK TTG8Q00A0E2S LINE #613.; [03] PARTS INFO ONLY. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - BOTH OVERWING SIDEWALL LIGHTS ARE NOT PROPERLY INSTALLED. ; / [01] ADJUSTED BOTH OVERWING SIDEWALL LIGHT COVERS PER AMM33-21-00.; [02] INSPECTED 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - PASSENGER CABIN FORWARD LOWERED CEILING PANEL EXIT SIGN TO FLIGHT ATTENDANT CALL INDICATOR LIGHT CLIP BROKEN. ; / [01] REMOVED AND REPLACED LIGHT ASSY. PER AMM 33-51-01<BR> OPS CHECK OK; [02] INSPECTED 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - THE 3 BELLY DRAINS AT STA 500B HAVE SURFACE CORROSION AROUND DRAIN ON THE EXTERNAL FUSELAGE. ; / [01] REMOVED LIGHT SURFACE CORROSION WITHIN LIMITS IAW SRM 53-30-01-1A-1.; [02] C/W NDT INSPECTION PER SRM 53-30-01-1A-1. AND 737 NDT PART 6 51-00-00 PROCEDURE 23.; [03] VERIFIED CORRECTIVE ACTION STEP #1; [04] ALODINED AND PRIMED BARE METAL IAW SRM 53-30-01-1A-1.; [05] REMOVED CORROSION PER SRM 51-10-02 .WITHIN LIMITS PER SRM 53-30-01-1A-1 SEE STEPS 1 THROUGH 4 FOR ADDITIONAL WORK PREFORMED 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - RIGHT EMERGENCY EXIT DOOR LIGHT LENS IS CRACKED AT AFT FASTENER. ; / [01] REMOVED AND REPLACED R/H EMERG. LIGHT LENS PERAMM 33-51-01; [02] INSPECTED WORK PERFORMED. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - LT WING I/B UPPER WING ROOT PANEL SUPPORT CLIP CRACKED ABOVE TANK 1 BOOST PUMP ; / [01] R/R SUPPORT CLIP PER SRM 51-40-02 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - FWD CARGO AFT R/H BULKHEAD LOWER CURVED 'L' ANGLE AT STA 500D HAS CORROSION LOWER END. (MARKED) ; / [01] FOUND TO BE OUTOF LIMITS PER SRM 53-30-08-1A-1.; [02] 1. DANIEL ANDERSON (TECHNICIAN); 11-JAN-2022 05:56 UTC<BR>FOUND TO BE OUT OF LIMITS PER SRM 53-30-08-1A-1. INSPECTED.; [03] LOCATED AND DRILL NEW R/H BULKHEAD ANGLE PER SRM 51-40-05.; [04] 3. DANIEL ANDERSON (TECHNICIAN); 11-JAN-2022 08:48 UTC<BR>LOCATED AND DRILL NEW R/H BULKHEAD ANGLE PER SRM 51-40-05. INSPECTED. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - FWD SERVICE DOOR ; BEAM #4 HAS CRACK INDICATION IN RADIUS AT INBOARD HOLE. REMOVED AND REPLACED R1 DOOR GUIDE ARM AND ROLLER PER AMM 52-41-21.; [03] REMOVED AND REPLACED R1 DOOR UPPER TORQUE TUBE LINK ASSEMBLY PER AMM 52-41-41.; [04] INSPECTED WORK PERFORMED IN C/A #2 & #3; [05] REMOVED AND REPLACED R1 DOOR PER AMM 52-41-00.; [06] RIGGED R1 DOOR PER AMM 52-41-00.; [07] APPLIED CIC TO R1 DOOR PER AMM 51-00-59.; [08] INSPECTED WORK PERFORMED IN C/A #7; [09] RIGGED FWD SERVICEDOOR (R-1) PER AMM 52-41-00.; [10] C/W; [11] C/W; [12] ALL INSPECTION WORK COMPLIED WITH. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - FWD CARGO TRANSITION ANGLE JUST AFT OF DOOR CUTOUT R/H HAS CORROSION ON NUMEROUS FASTENER HOLES BETWEEN STA 480+15 THRUSTA 500A. (MARKED) ; / [01] LOCATED AND DRILLED NEW TRANSITION ANGLE IAW SRM 53-40-01.; [02] LOCATED AND DRILLED NEW TRANSITION ANGLE IAW SRM 53-40-01. ANGLE ENAMELED AND INSTALLED ON ROUTINE CARD TTG8Q004G007.; [03] LOCATED AND DRILLED NEWTRANSITION ANGLE IAW SRM 51-40-02. ANGLE ENAMELED AND INSTALLED ON ROUTINE CARD TTG8Q004G007. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - FWD CARGO RT TRANSITION ANGLE HAS CORROSION AROUND NUMEROUS FASTENER HOLES BETWEEN BS 500A THRU 500D. REMOVED FWD CARGORH TRANS ANGLE FROM STA 500A TO 500D. OUT OF LIMITS PER SRM 53-00-53-1A-2. LOCATED AND BACK DRILLED HOLES IN NEW RH TRANSITION ANGLE FROM BS 500A TO 500D IAW SRM 51-40-05-0G-0. C/W INSPECTION STEPS 1-3. ALODINED AND PRIMED RT TRANSITION ANGLE FROM BS 500A TO 500D IAW SOPM 20-41-02. INSPECTED ALODINED AND PRIMED LH TRANSITION ANGLE FROM BS 396 TO 500D IAW SOPM 20-41-02. INSTALLED NUTPLATES ON RT TRANSITION ANGLE IAW 51-40-10-2R-0. APPLIED PAINT TO RH TRANS ANGLE IAW SOPM 20-41-02. INSTALLED REPLACEMENT TRANS ANGLE PER SRM 51-40-02. INSTALLED REPLACEMENT TRANS ANGLE IAW SRM 51-40-02. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - FWD CARGO STA 500D LOWER BULKHEAD 'L' ANGLE HAS CORROSION AROUND RBL 17 THRU RBL 22. (MARKED) ; / [01] REMOVED CORROSIONFOUND TO BE OUT OF LIMITS; INSTALL OF NEW P/N 143A9485Y35 WILL BE ACCOMPLISHED ON TTG8Q004G007 STEP 42 PER SRM 53-00-53AND 5330-E-16461-NG; [02] 1. MICHAEL STANLEY (TECHNICIAN); 11-JAN-2022 15:53 UTC<BR>REMOVED CORROSION FOUND TO BE OUT OF LIMITS; INSTALL OF NEW P/N 143A9485Y35 WILL BE ACCOMPLISHED ON TTG8Q004G007 STEP 42 PER SRM 53-00-53 AND 5330-E-16461-NG INSPECTED.; [03] REMOVED AND REPLACEMENT OF PART WILL BE ACCOMPLISHED ON TTG8Q004G007 STEP 42. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - FWD CARGO L/H TRANSITION ANGLE HAS CORROSION AROUND NUMEROUS FASTENER HOLES BETWEEN STA 500+14 THRU STA 500C+8. OUT OFLIMITS IAW SRM 53-00-53-1A-2.; REMOVED FWD CARGO LT TRANS ANGLE. LOCATED AND BACK DRILLED HOLES IN NEW LT TRANSITION ANGLE IAW SRM 51-40-05-0G-0. ALODINED AND PRIMED LT TRANSITION ANGLE IAW SOPM 20-41-02.; INSPECTED ALODINED AND PRIMED LTTRANSITION ANGLE IAW SOPM 20-41-02. INSTALLED NUTPLATES ON LT TRANSITION ANGLE IAW SRM 51-40-10-2R-0. APPLIED PAINT TO LT TRANS ANGLE IAW SOPM 20-41-02. INSTALLED REPLACEMENT LT TRANS ANGLE FWD CARGO WITH FASTENERS IAW SRM 51-40-02. INSTALLED REPLACEMENT LT TRANS ANGLE FWD CARGO WITH FASTENERS PER SRM 51-40-02. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - FWD CARGO SMALL TRANSITION ANGLE JUST FWD OF DOOR CUTOUT IS DEFORMED AFT END.(MARKED) ; / [01] LOCATED AND DRILLED NEW TRANSITION ANGLE PER SRM 53-40-01; [02] LOCATED AND DRILLED NEW TRANSITION ANGLE PER SRM 53-40-01.<BR>INSPECTION C/W.; [03] INSTALLED PER SRM 51-40-02; [04] INSTALLED PER SRM 51-40-02. INSPECTION C/W. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727C+14. ; / [01] R&R?D L/H TRANSITION ANGLE IAW SRM 51-40-02.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE AT STA.727B+6 ; / [01] LINE 13 IN MEASUREMENTS IS INCORRECTLY NA. IT SHOULD READ 155.5; [02] REMOVED AND REPLACED AFT CARGO R/H TRANSITION ANGLE FROM STA. 727TO STA 767; [03] REMOVED AND REPLACED AFT CARGO R/H TRANSITION ANGLE FROM STA. 727 TO STA 767 PER SRM 51-40-02; [04] INSPECTED. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727D+7. ; / [01] REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE IAW SRM 51-40-02.; [03] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [04] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADDFOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE FROM STA.727E TO STA.747. ; / [01] CORROSION FOUNDTO BE OUT OF LIMITS. ALL WORK DONE IAW SRM 53-00-53-1A-2.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.727C+6. ; / [01] R&R?D L/H TRANSITION ANGLEFROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [02] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.767+3. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED .007? ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE FROM STA.747 TO STA.767. ; / [01] CORROSION FOUNDTO BE OUT OF LIMITS; REMOVED .006? .ALL WORK DONE IAW SRM 53-00-53-1A-2.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+2. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS;M REMOVED .OO5? ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.767+7. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED .009?; ALL WORK DONE IAW SRM 53-00-53-1A-2; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847IAW SRM 51-40-02.; [03] INSPECTED. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+11. ; / [01] CORROSION FOUND TO BE OUTOF LIMITS. REMOVED .006?. ALL WORK DOWN IAW SRM 53-00-53-1A-2.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847 IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+14. ; / [01] CORROSION FOUND TO BE OUTOF LIMITS. REMOVED .008? ALL WORK DONE IAW SRM 53-00-53-1A-1.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. <BR>PLEASE ADD FOR ENGINEERING-MEASUREMENT 13 FINAL W (FROM WATER LINE 1 TO WATER LINE 2) 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT; RIGHT TRANSITION ANGLE HAS CORROSION AROUND FASTENER HOLE FROM STA.727D TO 727E' ; / [01] REMOVEDAND REPLACED AFT CARGO RIGHT TRANSITION ANGLE FROM STA. 727 TO STA. 767 PER SRM 51-40-02; [02] INSPECTED. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - AFT CARGO COMPARTMENT; LEFT TRANSITION CORROSION AROUND FASTENER HOLE AT STA.787+9. ; / [01] CORROSION FOUND TO BE OUT OF LIMITS; REMOVED .005?. ALL WORK DONE IAW SRM 53-00-53-1A-1.; [02] R&R?D L/H TRANSITION ANGLE FROM STA. 727 TO STA. 847IAW SRM 51-40-02.; [03] INSPECTED L/H TRANSITION ANGLE. 2022-03-02
N917WN BOEING 7377H4 During UNKNOWN - CRACK NOTED AT EXTERNAL POWER RECEPTICLE DOOR. / REPAIRED PER SRM 53-10-15-2R-4 SEE N/R D317613 FOR WORK ACCOMPLISHED. CL# 91269 DMA # 0074914 2022-03-01
N917WN BOEING 7377H4 During INSP/MAINT - REF. MX NOTE ON LOG PG 0338186 - CRACK NOTED ON ELECTRIC POWER RECEPTACLE DOOR FRAME. / REPAIRED PER SRM 53-10-15-2R-4 FIG. 203 ZONE 1. SEE. SAM 326 FOR INDIVIDUAL SIGN OFF. 2022-03-01
N917WN BOEING 7377H4 During INSP/MAINT - FWD CARGO R/H SIDEWALL TRANSITION ANGLE HAS CORROSION BETWEEN STA.500-500B / WP:E105601-WONG; JOHN - 12/02/2017 10:07 COMPLETE: REMOVE AND REPLACED FWD CARGO R/H SIDEWALL TRANSITION ANGLE BETWEEN STA.500-500B IAW SRM 53-00-53-2R-5 AND SEE BELOW FOR INDIVIDUAL SIGN OFFS. AND CHANGED CORROSION ITEMS. 2022-03-01
N917WN BOEING 7377H4 During INSP/MAINT - FWD CARGO L/H SIDEWALL TRANSITION ANGLE HAS CORROSION BETWEEN STA.500-500C. / REMOVED AND REPLACED DAMAGED SECTION OF TRANSITION ANGLE PER SRM 51-40-02 AND SRM 53-00-53-2R-5. 2022-03-01
N917WN BOEING 7377H4 During NOT REPORTED - LEFT HORIZONTAL LOWER STABILIZER SKIN HAS CRACK INDICATION ON RIB 193.90 ON INBOARD FASTENER ROW APPROX 16.5' FROM LEADING EDGE BETWEEN (2 RIVETS) ; / [01] GAINED ACCESS AND REMOVED DAMAGED AREA PER SRM 55-10-01-2R-11.; [02] HFEC VERIFIED DAMAGE REMOVAL PER NDT MANUAL 51-00-00 PROCEDURE 23 PART 6 .NO DEFECTS NOTED.; [03] PERFORMED HFEC INSPECTION OF EXISTINGHOLES IAW BOEING NDT 51-00-00 PT. 6 PROCEDURE 16. NO DEFECTS NOTED.; [04] FABRICATED LOCATED AND DRILLED REPAIR PARTS PER SRM 55-10-01-2R-11.; [05] INSPECTION C/W FABRICATED LOCATED AND DRILLED REPAIR (CA #4); [06] TREATED AND PRIMED REPAIR PARTS AND BARE SURFACES IN REPAIR AREA PER SRM 55-10-01-2R-11.; [07] INSPECTED THE PRIMED REPAIR PARTS AND BARE SURFAC 2022-02-01
N917WN BOEING 7377H4 During NOT REPORTED - LT WING WAFFLE PLATE CRACKED I/B #3 FLAP TRACK ; / [01] REMOVED FASTENERS PER SRM 51-40-02; [02] REMOVED AND REPLACED PER SRM 51-40-02.; [03] INSPECTION C/W R@R OF WAFFLE PLATE PER SRM 51-40-02 2022-02-01
N917WN BOEING 7377H4 During INSP/MAINT - LT WING I/B AFT FLAP WEDGE LOWER SURFACE HAS PLUG O/B AREA ; / [01] CLEANED AND PRIMED PER SRM 51-70-10 REPAIR #4.; CLEANED AND PRIMED PER SRM 51-70-10 REPAIR #4. OK TO INSTALL REPAIR.; [03] APPLIED REPAIR DOUBLER PER SRM 51-70-10; REPAIR #4.; APPLIED REPAIR DOUBLER PER SRM 51-70-10; REPAIR #4. INSPECTED.; [05] REPAIRED PER SRM 51-70-10;REPAIR #4; RESTORED FINISH PER M/M 51-21-99. 2022-02-01
N917WN BOEING 7377H4 During NOT REPORTED - R/H WING LOWER TRAILING EDGE WIGGLE PLATE PHENOLIC STRIP CRACKED IN TWO PLACES BETWEEN #7 AND #8 FLAP TRACK FAIRINGS APPROXIMATED ORSS 409 -440 (MARKED) ; / [01] REMOVED AND REPLACED R/H WING LOWER TRAILING EDGE WIGGLE PLATE BETWEEN #7 AND#8 FLAP TRACK FAIRINGS APPROXIMATED ORSS 409 -440 PER SRM 51-40-02; [02] C/W 2022-02-01
N917WN BOEING 7377H4 During NOT REPORTED - FORWARD CARGO DEPARTMENT FLOOR PANEL HAS DAMAGE ( REPORTED BY RAMP PERSONNEL) ; / [01] OK TO CONTINUE PER MEL25-16-01 SP1B. AUTH 21670 FWD CARGO INOP FOR USE; [02] R&R FWD CARGO FLOOR PANEL 120CF REF A.M.M 125-52-10<BR>THIS CLEARS MEL 25-16-01 2021-12-28
N917WN BOEING 7377H4 During NOT REPORTED - RH OVERWING EXIT FLUORESCENT LIGHT LENS CRACKED / LOG PAGE 1800653 R&R'D RH OVERWING EXIT FLOURESCENT LIGHT LENSE PER AMM 33-51-11 CL#77252 2021-07-16
N917WN BOEING 7377H4 During INSP/MAINT - IN FLIGHT DECK; PANEL BELOW L/H STAB TRIM WHEEL IS CRACKED / REMOVED AND REPLACED PER AMM 25-11-21. 2021-04-08
N917WN BOEING 7377H4 During NOT REPORTED - AFT SERVICE DOOR EXIT LIGHT COVER MISSING. R & R AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS, IAW M/M 33-51-01. 2021-01-05
N917WN BOEING 7377H4 During NOT REPORTED - FWD SERVICE DOOR UPPER HANDLE BROKEN. R&R ASSIST HANDLE BASE IAW AMM 52-41-31 2020-07-23
N917WN BOEING 7377H4 During UNKNOWN - EXIT SIGN COVER AT OVERWING EXIT ON CAPTAIN'S SIDE IS BROKEN. REPLACED LENS COVER PER AMM 33-51-03. 2020-07-16
N917WN BOEING 7377H4 During INSP/MAINT - AFT L/H DOOR EXIT SIGN HOUSING DAMAGED AT LOWER FORWARD SIDE. R&R SIGN HOUSING PER AMM. 2020-06-03
N917WN BOEING 7377H4 During INSP/MAINT - L/H EMERGENCY OVERHEAD BINS LIGHTS INOP AT POSITIONS 6 TO 12. RELAMPED LIGHT PER AMM. 2020-06-03
N917WN BOEING 7377H4 During INSP/MAINT - L/H OVERWING EMERGENCY EXIT SIGNS UPPER AND LOWER POSITION INOP. R&R POWER SUPPLY PER AMM. 2020-06-03
N917WN BOEING 7377H4 During INSP/MAINT - L/H OVERWING EMERGENCY EXIT SIGNS UPPER AND LOWER POSITION INOP. ACCOMPLISHED DISCREPANCY ON N/R 2015426/ 1000/ 0148 2020-06-03
N917WN BOEING 7377H4 During INSP/MAINT - L/H AFTER WING EMERGENCY ESCAPE LIGHTS INOP. R&R POWER SUPPLY M1670 IAW AMM. 2020-06-03
N917WN BOEING 7377H4 During INSP/MAINT - EMERGENCY EXIT LIGHT ASSEMBLY CRACKED AT CEILING PANEL ABOVE SEAT ROW 11. R&R LIGHT ASSEMBLY PER AMM. 2020-06-03
N917WN BOEING 7377H4 During NOT REPORTED - L1 DOORS EMERGENCY EXIT SIGN INOP. CLEANED CONNECTOR AT BATTERY PACK M1674 PER AMM. 2020-06-03
N917WN BOEING 7377H4 During INSP/MAINT - R/H AFTER WING EMERGENCY ESCAPE LIGHTS INOP. R&R POWER SUPPLY M1670 IAW AMM. 2020-06-03
N917WN BOEING 7377H4 During INSP/MAINT - R/H EMERGENCY OVERHEAD BINS LIGHTS INOP AT POSITIONS 3 TO 6. / RELAMPED LIGHT PER AMM. 2020-06-03
N917WN BOEING 7377H4 During INSP/MAINT - L/H OVERWING EMERGENCY EXIT SIGNS UPPER AND LOWER POSITION INOP. R&R BATTERY PACK PER AMM. 2020-06-03
N917WN BOEING 7377H4 During NOT REPORTED - R1 DOORS EMERGENCY EXIT SIGN INOP. / CLEANED CONNECTOR AT BATTERY PACK M1674 PER AMM. 2020-06-03
N917WN BOEING 7377H4 During INSP/MAINT - AFT CARGO COMPARTMENT FLOOR STRUCTURE L/H ZEE CHANNEL CORRODED SPOTS BETWEEN BS. 727D TO BS. 827. / R&R ZEE CHANNEL IAWSRM AND DWG. 2020-05-27
N917WN BOEING 7377H4 During INSP/MAINT - FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 21L. / R&R GUSSET PER SRM AND DWG. 2020-05-26
N917WN BOEING 7377H4 During INSP/MAINT - L/H BODY FAIRING ATTACH FRAME CRACKED AT BS. 520, STR. 20L. / R&R FRAME PER SRM AND DWG. 2020-05-26
N917WN BOEING 7377H4 During INSP/MAINT - AFT CARGO COMPARTMENT FLOOR STRUCTURE R/H ZEE CHANNEL CORRODED BETWEEN BS. 727E TO BS. 787. / R&R "Z" CHANNEL IAW SRM & DWG. 2020-05-21
N917WN BOEING 7377H4 During INSP/MAINT - FORWARD CARGO HAD GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET PER SRM. 2020-05-21
N917WN BOEING 7377H4 During INSP/MAINT - FORWARD CABIN FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS. 380 TO BS. 400, BL 0. / R&R INTERCOSTAL IAW SRM. 2020-05-13
N917WN BOEING 7377H4 During INSP/MAINT - MAIN CABIN FLOOR SUPPORT INTERCOSTAL UPPER ANGLE CRACKED BETWEEN BS. 500D TO BS. 520, APPROXIMATELY BL 0. / R&R ANGLE PER SRM. 2020-05-13
N917WN BOEING 7377H4 During INSP/MAINT - L/H HORIZONTAL STABILIZER RIB ASSEMBLY 4 STAB. STA. 120.30 STIFFENER #3 CRACKED. / REPAIR #4 RIB PER SRM. 2020-05-13
N917WN BOEING 7377H4 During NOT REPORTED - FORWARD SERVICE DOOR EXIT SIGN LENS HAD COME OFF. / REPAIRED LENS PER EA. 2020-04-30
N917WN BOEING 7377H4 During INSP/MAINT - GROUND POWER DOOR FRAME SKIN CRACKED AFT OF DOOR. / REPAIRED SKIN PER SRM. 2020-03-05
N917WN BOEING 7377H4 During INSP/MAINT - LT PHOTOLUMINESCENT STRIP DAMAGED, 1ST SECTION. R&R STRIP REF AMM. 2020-01-14
N917WN BOEING 7377H4 During INSP/MAINT - RT PHOTOLUMINESCENT STRIP DAMAGED, 1ST SECTION. R&R STRIP REF AMM. 2020-01-14
N917WN BOEING 7377H4 During INSP/MAINT - L1 EMERGENCY LIGHT INOP. RELAMPED BULB PER MM. 2019-12-31
N917WN BOEING 7377H4 During UNKNOWN - R2 DOOR EMERGENCY SLIDE CONTAINER LOOSE. SECURED DOOR IAW SIP. 2019-03-21
N917WN BOEING 7377H4 During INSP/MAINT - R2 DOOR EXTERIOR EMERGENCY ESCAPE LIGHT INOP. RELAMPED LIGHT PER AMM. 2019-03-01
N917WN BOEING 7377H4 During INSP/MAINT - LT OVERWING EMERGENCY ESCAPE LIGHT INOP. RELAMPED LIGHT PER AMM. 2019-03-01
N917WN BOEING 7377H4 During CLIMB - ANTI-SKID INOPERATIVE LIGHT INTERMITTENTLY CAME ON DURING CLIMB OUT. R & R THE NR 3 TRANSDUCERS IAW AMM. 2018-11-30
N917WN BOEING 7377H4 During NOT REPORTED - RIGHT OVERWING EXIT SIGN LIGHT CAP LOWER LEFT SIDE MISSING. INSTALLED THE LENS IAW AMM. 2018-10-31
N917WN BOEING 7377H4 During INSP/MAINT - RIGHT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE TRUNNION FITTING IAW EA. 2018-10-05
N917WN BOEING 7377H4 During INSP/MAINT - RIGHT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE TRUNNION FITTING IAW EA. 2018-09-28
N917WN BOEING 7377H4 During INSP/MAINT - LEFT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE FITTING CORRODED. REPAIRED THE TRUNNION FITTING IAW EA. 2018-09-28
N917WN BOEING 7377H4 During INSP/MAINT - FLOOR SUPPORT CRACKED AT BS 540, LBL 1. R & R THE FLOOR SUPPORT IAW SR. 2018-04-02
N917WN BOEING 7377H4 During INSP/MAINT - AFT CARGO COMPARTMENT FLOOR PANEL SPLICE STRAP CORRODED AT BS 767+6, RBL 19. R&R SPLICE TEE ASSEMBLY PER SRM. 2017-12-04
N917WN BOEING 7377H4 During INSP/MAINT - AFT CARGO COMPARTMENT FLOOR PANEL SPLICE STRAP CORRODED AT BS 887, RBL 16. R&R SPLICE TEE ASSEMBLY PER SRM. 2017-12-04
N917WN BOEING 7377H4 During INSP/MAINT - L2 DOOR EMERGENCY EXIT SIGN MISSING DIRECTIONAL ARROW. R & R THE SIGN IAW MM. 2017-02-08
N917WN BOEING 7377H4 During INSP/MAINT - L2 DOOR EMERGENCY SLIDE GIRT BAR PLASTIC STOP MISSING. INSTALLED THE PIN IAW SIP. 2017-01-18
N917WN BOEING 7377H4 During UNKNOWN - RT LOWER EMERGENCY EXIT LIGHT LENS COVER MISSING. INSTALLED COVER PER MM. 2016-11-30
N917WN BOEING 7377H4 During DESCENT - DIVERSION, DECLARED EMERGENCY, LOSS OF CABIN PRESSURE AT 38,000 FT INITIATED EMERGENCY DESCENT. LANDED, R & R NR 1 LT PACK VALVE IAW AMM. 2016-08-22
N917WN BOEING 7377H4 During CRUISE - CABIN ALTITUDE WARNING HORN AND LIGHT INDICATION. EMERGENCY DECLARED AND DIVERTED. R & R THE NR 1 CABIN PRESSURE CONTROLLER IAW MM. 2016-08-02
N917WN BOEING 7377H4 During CRUISE - CABIN ALTITUDE WARNING HORN AND LIGHT INDICATION. EMERGENCY DECLARED AND DIVERTED. R & R THE OUTFLOW VALVE IAW MM. 2016-08-02
N917WN BOEING 7377H4 During UNKNOWN - R2 DOOR GALLEY EXIT SIGN LENS COVER LOOSE. R & R COVER IAW AMM. 2016-06-24
N917WN BOEING 7377H4 During UNKNOWN - FORWARD SERVICE DOOR EMER EXIT SIGN BROKEN LENS. R & R BASE ASSEMBLY IAW AMM. 2016-05-17
N917WN BOEING 7377H4 During UNKNOWN - OVERHEAD EMER EXIT SIGN LOOSE. SECURED SIGN IAW MM. 2016-04-26
N917WN BOEING 7377H4 During INSP/MAINT - RIGHT HORIZONTAL STABILIZER RIB CRACKED, STAB. STATION 166.30 AT FWD SPAR OTBD FASTENER. REPAIRED RIB IAW SRM. 2016-01-22
N917WN BOEING 7377H4 During INSP/MAINT - RIGHT PAX CABIN PHOTO LUMINESCENT STRIP WORN. R & R STRIP IAW MT. 2016-01-22
N917WN BOEING 7377H4 During INSP/MAINT - LEFT PAX CABIN PHOTO LUMINESCENT STRIP WORN. R & R STRIP IAW MT. 2016-01-22
N917WN BOEING 7377H4 During INSP/MAINT - FORWARD GALLEY THRESHOLD SUPPORT ANGLE, CORRODED AT BS 299, RBL 54. R & R ANGLE IAW SRM. 2016-01-19
N917WN BOEING 7377H4 During INSP/MAINT - AFT CARGO FLOOR SUPPORT, CORRODED AT BS 767. R & R SUPPORT IAW SRM. 2016-01-19
N917WN BOEING 7377H4 During INSP/MAINT - AFT GALLEY FLOOR, STRUCTURE WEB STRAP CORRODED, BETWEEN BS 1016 - 1030, LBL 3. R & R WEB STRAP IAW SRM. 2016-01-19
N917WN BOEING 7377H4 During INSP/MAINT - FORWARD GALLEY DOOR, Z ANGLE ON OTBD SIDE CRACKED AT BS 294.5, RBL 53. R & R Z ANGLE IAW SRM. 2016-01-19
N917WN BOEING 7377H4 During INSP/MAINT - AFT GALLEY FLOOR, STRUCTURE WEB STRAP CORRODED, BETWEEN BS 1016 - 1030, RBL 3. R & R WEB STRAP IAW SRM. 2016-01-19
N917WN BOEING 7377H4 During INSP/MAINT - FORWARD GALLEY DOOR, Z ANGLE ON INBD SIDE CRACKED, BETWEEN BS 294.5 - 328, RBL 54. R & R ANGLE IAW SRM. 2016-01-19
N917WN BOEING 7377H4 During INSP/MAINT - AFT CARGO THRESHOLD BEAD WEB CORRODED. R & R WEB IAW SRM. 2016-01-19
N917WN BOEING 7377H4 During INSP/MAINT - FORWARD ENTRY DOOR, Z ANGLE CRACKED AT FASTENER HOLE AT BS 303.9. R & R Z ANGLE IAW SRM. 2016-01-19
N917WN BOEING 7377H4 During INSP/MAINT - FORWARD CARGO SUPPORT, Z ANGLE CORRODED BETWEEN BS 485 - 500D. R & R Z ANGLE IAW SRM. 2016-01-19
N917WN BOEING 7377H4 During INSP/MAINT - WHEEL WELL DECK CRACKED AT BS 663, BETWEEN RBL 32.5 TO LBL 33, 4" FROM TOP OF FUEL TANK. REPAIRED DECK IAW SRM. 2016-01-14
N917WN BOEING 7377H4 During INSP/MAINT - WHEEL WELL DECK CRACKED AT BS 663, BETWEEN LBL 33.5 - LBL 34.75, 4" BELOW THE WW DECK. REPAIRED DECK IAW SRM. 2016-01-14
N917WN BOEING 7377H4 During DESCENT - DIVERSION, FLIGHT ATTENDANT REPORTED SOUND & ODOR MID CABIN. TURNED RECIRCULATING FAN OFF & SMELL DISSIPATED. R & R RECIRCULATING FAN IAW MM. 2015-02-26
N917WN BOEING 7377H4 During INSP/MAINT - LONGITUDINAL FLOORBEAM FWD OTBD HOLE CRACKED AT BS 727B, LBL 45. REPAIRED BEAM IAW EA. 2015-01-23
N917WN BOEING 7377H4 During INSP/MAINT - LONGITUDINAL FLOORBEAM AFT OTBD HOLE CRACKED AT BS 727B, LBL 45. REPAIRED BEAM IAW EA. 2015-01-23
N917WN BOEING 7377H4 During INSP/MAINT - LONGITUDINAL FLOORBEAM FWD INBD HOLE CRACKED AT BS 727B, LBL 45. REPAIRED BEAM IAW EA. 2015-01-23
N917WN BOEING 7377H4 During INSP/MAINT - LONGITUDINAL FLOORBEAM UPPER AFT END CRACKED AT BS 727B, LBL 45. REPAIRED BEAM IAW EA. 2015-01-23
N917WN BOEING 7377H4 During UNKNOWN - FORWARD FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM. 2015-01-14
N917WN BOEING 7377H4 During UNKNOWN - R1 DOOR EMER EVAC SLIDE GIRT HOLDER BAR DIRTY. CLEANED HOLDER IAW AMM. 2014-12-05
N917WN BOEING 7377H4 During INSP/MAINT - FORWARD ENTRY EMER BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM & DWG. 2014-12-03
N917WN BOEING 7377H4 During INSP/MAINT - SERVICE ENTRY EMER BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM & DWG. 2014-12-02
N917WN BOEING 7377H4 During UNKNOWN - OVERWING EXIT SIGN BROKEN. R & R SIGN IAW AMM. 2014-11-18
N917WN BOEING 7377H4 During UNKNOWN - R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK IAW SRM. 2014-05-20
N917WN BOEING 7377H4 During INSP/MAINT - R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUSTMENT. ADJUSTED GIRT BAR IAW MM. 2014-03-18
N917WN BOEING 7377H4 During INSP/MAINT - L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINER COLLAR CRACKED. R 7 R GIRT BAR STOP IAW MM. 2014-03-18
N917WN BOEING 7377H4 During INSP/MAINT - R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR RETAINER CLIP LOOSE. SECURED CLIP IAW SRM. 2014-03-17
N917WN BOEING 7377H4 During INSP/MAINT - CABIN FLOOR INTERCOSTAL CRACKED AT BS 540, BETWEEN BL 0 TO RBL 24. REPAIRED INTERCOSTAL IAW SRM. 2014-03-17
N917WN BOEING 7377H4 During UNKNOWN - RT OVERWING EMERGENCY EXIT LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW MM. 2014-02-18
N917WN BOEING 7377H4 During INSP/MAINT - LEFT EEPLS COVER CRACKED BETWEEN ROW 2 TO ROW 11. REMOVED AND REPLACED COVER PER MM. 2012-12-19
N917WN BOEING 7377H4 During INSP/MAINT - LEFT EEPLS LENS CRACKED AT ROW 23. REMOVED AND REPLACED LENS PER MM. 2012-12-17
N917WN BOEING 7377H4 During INSP/MAINT - LEFT EEPLS LENS CRACKED AT ROW 12. REMOVED AND REPLACED LENS PER MM. 2012-12-17
N917WN BOEING 7377H4 During INSP/MAINT - R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2012-12-17
N917WN BOEING 7377H4 During INSP/MAINT - L1 DOOR EMERGENCY EVAC SLIDE COVER LENS LOOSE. SECURED LENS PER MM AND MT. 2012-12-17
N917WN BOEING 7377H4 During INSP/MAINT - R2 DOOR EMERGENCY EVAC SLIDE COVER LENS LOOSE. SECURED LENS PER MM AND MT. 2012-12-17
N917WN BOEING 7377H4 During INSP/MAINT - L1 DOOR EMERGENCY SLIDE FELL OUT OF CONTAINER (STILL OPERABLE). REINSTALLED SLIDE PER MM. 2012-09-12
N917WN BOEING 7377H4 During INSP/MAINT - R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINER HOOK LOOSE. SECURED HOOK ASSY PER SRM. 2012-09-11
N917WN BOEING 7377H4 During INSP/MAINT - L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR AFT RETAINER HOOK LOOSE. SECURED HOOK ASSY PER SRM. 2012-09-11
N917WN BOEING 7377H4 During UNKNOWN - L2 DOOR EMERGENCY EVAC SLIDE COVER LENS CRACKED. REMOVED AND REPLACED LENS PER M/M & MT. 2012-09-11
N917WN BOEING 7377H4 During INSP/MAINT - EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED COVER PER MM. 2012-06-29
N917WN BOEING 7377H4 During INSP/MAINT - RT CABIN BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACKS PER M/M. 2012-06-04
N917WN BOEING 7377H4 During INSP/MAINT - LT CABIN BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACKS PER M/M. 2012-06-04
N917WN BOEING 7377H4 During INSP/MAINT - EGRESS LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER M/M. 2012-04-23
N917WN BOEING 7377H4 During UNKNOWN - L1 DOOR EEPLS COVER MISSING. REMOVED AND REPLACED COVER PER MM. 2012-03-22
N917WN BOEING 7377H4 During UNKNOWN - EEPLS LENS MISSING AT ROW 1. INSTALLED LENS PER MM. 2012-03-05
N917WN BOEING 7377H4 During INSP/MAINT - DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 20. REMOVED AND REPLACED LENS PER MM. 2011-06-17
N917WN BOEING 7377H4 During INSP/MAINT - DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM. 2011-04-01
N917WN BOEING 7377H4 During INSP/MAINT - R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM. 2011-02-18
N917WN BOEING 7377H4 During INSP/MAINT - DURING SCHEDULED MV1 CHECK, FOUND LT EELS LENS MISSING AT ROW 8. INSTALLED LENS PER MM. 2011-01-26
N917WN BOEING 7377H4 During INSP/MAINT - DURING SCHEDULED HC1 CHECK, FOUND FWD EEPLS END CAP MISSING. INSTALLED END CAP PER MM. 2010-04-06
N917WN BOEING 7377H4 During INSP/MAINT - FWD EEPLS LOOSE. SECURED EEPLS PER MM. 2010-03-16
N917WN BOEING 7377H4 During INSP/MAINT - EMERGENCY EXIT LIGHT LENS COVER LOOSE. REMOVED AND REPLACED COVER PER MM. 2010-02-24
N917WN BOEING 7377H4 During INSP/MAINT - FWD CABIN EEPLS LOOSE. SECURED EEPLS PER MM. 2010-01-06
N917WN BOEING 7377H4 During INSP/MAINT - FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM. 2009-12-15
N917WN BOEING 7377H4 During DESCENT - AT START OF DESCENT INTO TUL - FLT ATTENDANT CALLED AND COMPLAINED OF ODOR SIMILAR TO BURNING RUBBER MID CABIN, NO SMOKE. TURNED OFF RECIRC FAN AND ODOR WENT AWAY. REMOVED AND REPLACED RECIRC FAN PER MM. 2009-07-28
N917WN BOEING 7377H4 During INSP/MAINT - L1 DOOR LOWER EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM. 2009-03-20
N917WN BOEING 7377H4 During INSP/MAINT - R2 DOOR EMERGENCY EVAC SLIDE FELL OUT OF IT'S CONTAINER, DID NOT DEPLOY. REINSTALLED SLIDE PER MT. 2008-12-23
N917WN BOEING 7377H4 During INSP/MAINT - DURING SCHEDULED MV1 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM. 2008-04-23

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Aviation Datasets Explained


Aircraft Lookup allows anyone to quickly search public datasets published by various aviation administrative services as well as marketplaces and other private aviation data providers in the United States. These datasets provide valuable insight into the history and maintenance record of any aircraft registered in the US. When you provide an N-Number above, we cross reference historical SDR, FAA, and NTSB datasets to identify any relevant records related to that N-Number.

As you may be aware, N-Numbers are not connected to an aircraft for the life of that aircraft - N-Numbers may be deregistered, and re-registered to completely different aircraft. For that reason, please confirm that the details of any search result correspond to the make and model you intended to pull records for.

SDR, FAA, and NTSB databases are provided as follows:

The Service Difficulty Reports (SDR) dataset is defined as "[t]he reports submitted by certificate holders and certificated repair stations, known as service difficulty reports (SDR's), provide the FAA with airworthiness statistical data necessary for planning, directing, controlling, and evaluating certain assigned safety-related programs." This data is, in its raw form, a tab-delimited file with encoded field headers.

The FAA Registration dataset is fairly straightforward - it is a listing of current registrations (along with addresses, aircraft serial number, and other basic metadata) at any point in time. The registration data is a comma delimited file that has named fields at the top of each file. The FAA provides historical data on their site for the previous few years.

The FAA Accident/Incident dataset covers a range of accidents and incidents that may or may not overlap with NTSB data. Typically, more significant crashes are covered by NTSB data while less significant crashes are more comprehensively covered by the FAA Accident/Incident data, which will frequently include minor events like gear-up landings and so forth. The data provided by the FAA is in a tab-delimited file with encoded field headers.

The NTSB investigation dataset is distinct from the FAA dataset. While the number of accidents or incidents they cover are less numerous, the depth at which they are covered is significantly deeper when reported by the NTSB. While each record from the NTSB contains incredible amounts of metadata related to people responsible for the flight, prevailing meteorological conditions at the time of flight, and passengers aboard, this aircraft lookup tool only provides basic summary data. The full dataset is provided as a series of Microsoft access file databases on the NTSB site.