Aircraft Report for n8607m



Registration History for n8607m









N-Number Make Model Serial Location Description Time
N8607M BOEING 737-8H4 36634 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2013-01-19, expiration date 2025-02-28, serial number 36634. 2021-11-24
N8607M BOEING 737-8H4 36634 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2013-01-19, expiration date 2022-02-28, serial number 36634. 2019-02-04
N8607M BOEING 737-8H4 36634 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2013-01-19, expiration date 2022-02-28, serial number 36634. 2018-12-15
N8607M BOEING 737-8H4 36634 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2013-01-19, expiration date 2019-02-28, serial number 36634. 2015-12-10
N8607M BOEING 737-8H4 36634 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2013-01-19, expiration date 2019-02-28, serial number 36634. 2015-12-10
N8607M BOEING 737-8H4 36634 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2013-01-19, expiration date 2016-02-29, serial number 36634. 2013-02-04
N8607M BEECH P35 D-7231 PARKDALE, OR Aircraft registered to RAINBOW RANCH, serial number D-7231. 1983-04-09
N8607M BOEING 737-8H4 36634 SEATTLE, WA Aircraft registered to BOEING COMPANY, serial number 36634. 2012-07-09

Accident History for n8607m


N-Number Make Model Location Description Time
N8607M BEECH B35 MONARCH PASS, CO ENTERED ICING AND TURBULENCE IN SNOW-STORM IN MOUNTAIN AREA. LOST CONTROL. EXCEEDED DESIGN LOAD. AIRFRAME FAILED. 1981-03-06

Service Difficulty Reports for n8607m
























































































































N-Number Make Model Serial Description Time
N8607M BOEING 7378H4 During INSP/MAINT - EMERGENCY BATTERY PACK INOP AT STA 500C+7 / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACK AT STA 500C+7 PER AMM 33-51-06. OPS CHECK GOOD. 2022-07-14
N8607M BOEING 7378H4 During INSP/MAINT - FWD CARGO COMPARTMENT L/H SIDE LONGEST FLOOR TO SIDEWALL TRANSITION STRIP IS CORRODED ON BOTH TOP AND BOTTOM SIDES IN SEVERAL AREAS AS MARKED / EVALUATED DAMAGE. TOTAL ACCUMULATE CORROSION IS MORE THAN 20 INCHES. OUT OF LIMITS PER SRM 53-00-53-1A-1. VERIFIED NEW PART P/N 453A1611-16; ATAG ZK0028 I/A/W AIPC 25-52-10-03 ITEM 365 AT FORWARD CARGO COMPARTMENT L/H SIDE LONGEST FLOOR TO SIDEWALL TRANSITION STRIP 2022-03-14
N8607M BOEING 7378H4 During INSP/MAINT - FWD CARGO COMPARTMENT R/H SIDE FLOOR TO SIDEWALL TRANSITION; 2 EA STRIPS ARE CORRODED IN SEVERAL AREAS ON THE TOP AND BOTTOM SIDES AS MARKED / EVALUATED DAMAGE. TOTAL ACCUMULATED CORROSION LENGTH IS MORE THAN 20 INCHES. OUT OF LIMITS PER B737 SRM 53-00-53-1A-1. VERIFIED NEW PARTS: P/N 453A1611-5; ATAG A80157 AND P/N 453A1611-31 ATAG ZK0026 I/A/W AIPC 25-52-10-03 2022-03-14
N8607M BOEING 7378H4 During INSP/MAINT - FWD CARGO COMPARTMENT FWD FLOOR PNL 120AF IS CORRODED ON TOP SKIN SURFACE ON CORNER EDGE THE WIDTH OF BOARD AS MARKED /EVALUATED CORROSION DAMAGE ON FWD CARGO COMPARTMENT FLOOR PANEL 120AF AND FOUND IT OUT OF LIMITS IAW B737 SRM 53-00-53-1A-1. DAMAGE IS OVER ALLOWAWBLE LIMIT OF 20' IN LENGHT. REPLACED PANEL WITH NEW IAW IPC 25-52-1017. P/N: 453A1610-14. PANEL TO BE INSTALLED ON DOC # SAM-565S; W/O: 388785. A TAG: WN2860. 2022-03-14
N8607M BOEING 7378H4 During INSP/MAINT - FWD CARGO COMPARTMENT FLOOR PNL 120BF BOTOM SKIN SURFACE AREA HAS SEVRAL AREAS OF PROTECTIVE FINISH DETERIOATED / EVALUATED DAMAGE. FOUND CORROSION AT MULTIPLES LOCATIONS; DAMAGE LENGTH IS MORE THAN 20 INCHES; FOUND TO BE OUT OF LIMITS PERB737 SRM 53-00-53-1A-1. VERIFIED NEW PART P/N 453A1610-16 SI # 4251046 I/A/W AIPC 25-52-10-17 ITEM 15 AT FORWARD CARGO COMPARTMENT FLOOR PANEL 120BF 2022-03-14
N8607M BOEING 7378H4 During INSP/MAINT - FWD CARGO COMPARTMENT FLOOR PNL 120CF TOP SIDE L/H; R/H AND FWD EDGE OF PNL IS CORRODED AS MARKED / EVALUATED DAMAGE. TEDLAR ACCUMULATED CORROSION LENGTH IS MORE THAN 20 INCHES; OUT OF LIMITS PER B737 SRM 53-00-53-1A-1; VERIFIED NEW PART; P/N 453A1610-103. SI # 4251047; ATAG ZK0037 I/A/W AIPC 25-52-10-17 ITEM 25; AT FORWARD CARGO COMPARTMENT FLOOR PANEL 120CF 2022-03-14
N8607M BOEING 7378H4 During INSP/MAINT - FWD CARGO COMPARTMENT FLOOR PNL 120DF TOP SKIN SURFACE L/H; R/H AND FWD SIDES IS CORRODED AND 1 EA SPOT ON BOTTOM SIDE AS MARKED / EVALUATED CORROSION DAMAGE ON FWD CARFO COMPARTMENT FLOOR PANEL 120DF AND FOUND IT OUT OF LIMITS IAW B737 SRM53-00-53-1A-1. DAMAGE IS OVER ALLOWABLE LIMIT OF 20' IN LENGHT. REPLACED PANEL WITH NEW; P/N: 453A1610-20; IAW IPC 25-52-10-17. PANEL TO BE INSTALLED ON DOC #SAM-565S W/U: 388785 A TAG: AN1266. 2022-03-14
N8607M BOEING 7378H4 During INSP/MAINT - AFT PIT PANEL 140DF IS CORRODED / RECEIVED NEW AFT PIT PANEL PN#453A2610-20 IAW IPC 25-52-10-19 BECAUSE ORIGINAL PANEL FOUND TO BE OUT OF LIMITSIAW SRM 53-00-53-1A-1 OF MORE THAN 10INCHES OF CORROSION A-TAG #WN140DF 2022-03-14
N8607M BOEING 7378H4 During INSP/MAINT - AFT PIT PANEL 140AF IS CORRODED / REMOVED CORROSION ON PANEL 140AF FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 (MORETHAN 10') RECEIVED NEW AFT CARGO PANEL 140AF P/N 453A7610-38 SI #4251041 TAG# WN997 IAW IPC 25-52-10-19. PANEL 140AF WILL BE INSTALL ON W/O #38794/ 1000/0020 (CUSTOMER CARD # SA-M 5663 ACCOMPLISHMENT. 2022-03-14
N8607M BOEING 7378H4 During INSP/MAINT - AFT PIT PANEL 140EF IS CORRODED / RECIVED NEW AFT PIT PANEL PN #453A2610-58 IAW IPC 25-52-10-19 BECAUSE ORIGINAL PANEL FOUND TO BE OUT OF LIMITS.IAW SRM 53-00-53-1A-1 OF MORE THAN 10 INCES OF CORROSION A-TAG# ZK0036 PN#140EF 2022-03-14
N8607M BOEING 7378H4 During INSP/MAINT - AFT PIT PANEL 140CF IS CORRODED / RECEIVED NEW AFT PIT PANEL PN# 453A2610 IAW IPC 25-52-10-19 BECAUSE ORIGINAL PANEL FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 OF MORE THAN 10INCHES OF CORROSION A-TAG PANEL #140CF PN #453A2610-18 A-TAG# WN0558 2022-03-14
N8607M BOEING 7378H4 During INSP/MAINT - AFT PIT PANEL 140BF IS DENTED AND CORRODED / REMOVED CORROSION ON PANEL 140BF FOUND TO BE OUT OF LIMITS IAW SRM 53-0-53-1A-1 (MORE THEN 10 INCHES) RECEIVED NEW AFT PANEL 140BF P/N 453A2610-32 SI# 7253513 TAG# WN1363 IAW IPC 25-42-10-19. PANEL WILL BE INSTALL ON W/O #38794/ 1000/ 0020 (CUSTOMER CARD # SA-M 5655 ACCOMPLISHMENT). 2022-03-14
N8607M BOEING 7378H4 During INSP/MAINT - AFT CARGO COMPARTMENT BETWEEN STA 767 AND 787 R/H FLOOR SHIELD IS CORRODED TOP AND BOTTOM SIDES AS MARKED / REMOVED ANDREPLACED AFT CARGO PIT SHIELD R/H SIDE STA 767 TO 787 IAWE BOEING 737 SRM 51-40-02; BOEING DWSG 146A0081. REV A. TOOL AAR 1708 DUE 04-02-19 2022-03-14
N8607M BOEING 7378H4 During INSP/MAINT - AFT CARGO COMPARTMENT BETWEEN STA 767 AND 787 RBL 18.50 TRANSITION FLOOR PNL STRIP IS CORRODED / REMOVED CORROSION ON TRANSITION FLOOR PNL STRIP FOR AFT CARGO BETWEEN STA 767-787 IAW SRM 51-10-02-0G-0 NO LIMITS WERE NOTED IN THESRM (REPLACEPART) REPLACED AFT CARGO TRANSITION FLOOR PNL STRIP BETWEEN STA 767-787 IAW BOEING DWG #146A9401 REV C. (P/N-146A9401-4) (SI#3530573) TAG# WN8493 2022-03-14
N8607M BOEING 7378H4 During INSP/MAINT - FWD CARGO COMPARTMENT STA 500I LBL 24 TO RBL 24 FLOORBOARD AND AFT BULKHEAD SUPPORT ANGLE HAS CORROSION AS MARKED. / EVALUATED CORROSION IN FWD CARGO COMPARTMENT AT STA 500I; LBL 24 TO RBL 24 100% MATERIAL LOSS OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED BULK HEAD SUPPORT ANGLE IAW SRM 51-40-02-0G-0 AND BOEING DWG #143A9481 REV A 2022-03-14
N8607M BOEING 7378H4 During UNKNOWN - FWD LH EMERGENCY LIGHTS INOP ; / [01] REMOVED AND REPLACED FWD LH BATTERY PACK IAW AMM 33-51-06. 2022-03-09
N8607M BOEING 7378H4 During INSP/MAINT - FOUR EMERGENCY LIGHTS ON R/H SIDE OF A/C INOP (TWO AISLE AND TWO EXTERIOR). / [01] R&R BATTERY BACK M1671 OPS CK GOOD REF AMM 33-51-06 2022-03-09
N8607M BOEING 7378H4 During INSP/MAINT - RT WING TRAILING EDGE PANEL ATTACH WIGGLE PLATE CRACKED AT 19' OTBD OF SAIL TAIL. / REMOVED ON RT WING TRAILING EDGE PANEL ATTACH WIGGLE PLATE CRACKED NO FOUND ALOOWABLE DAMAGED ON THE SRM NOTES AND INSTALLED NEW ANGLE P/N 115A3750-18 ISSUETAG # A79425 IAW B737-800 SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AMM 51-21-91-620-802; DWG# 115A3700 REV- AND DWG#115A3760 REV:B (AT 19' OTBD OF SAIL TAIL) 2022-02-25
N8607M BOEING 7378H4 During INSP/MAINT - WING TO BODY FAIRING #193AL; UPPER SIDE OF PANEL; COMPOSITE MATERIAL WORN / PITTED ON I/B EDGE OF FAIRING; MARKED IN BLACK / REPAIRED WEAR DAMAGE ON INNER SURFACE OF PANEL 193AL IAW 737-800 SRM 53-60-70-1A-1 REV 71; SRM 51-70-08-0G-0 REV. 71. RESTORED FINISH IAW 737 AMM 51-21-81-370-802 REV. 72. 2022-01-26
N8607M BOEING 7378H4 During NOT REPORTED - AFT GALLEY EMER EXIT LIGHT SWITCH IS ILLUMINATED RED / PERFORMED FIM 33-50 TASK 801. OPERATIONAL CHECK OF EMERGENCY LIGHTS NORMAL. IT WAS INTERMITTENT FAULT. 2022-01-14
N8607M BOEING 7378H4 During INSP/MAINT - AFT EQUIPMENT COMPARTMENT DOOR HANDLE CRACKED / REMOVED AND REPLACED AFT EQUIPMENT COMPARTMENT DOOR HANDLE PER CMM 52-48-13INSP 50310 2021-12-30
N8607M BOEING 7378H4 During INSP/MAINT - R2 DOOR PNL 844DZ; LWR INNER FLANGE IS DAMAGED/DISTORTED / REPLACED R2 DOOR PNL 844DZ IAW AIPC 52-41-31-10 PAGE 11 ITEM#405. WN1771 2021-12-27
N8607M BOEING 7378H4 During INSP/MAINT - WET AREA FLOORBOARD 241AAF TOP SURFACE PLY IS DAMAGED IN SEVERAL AREAS. / REPLACED FLOOR BOARD 241AAF BY FABRICATION PERSAMPLE AND 737-800 SRM 53-00-50-2R-0 REPAIR GENERAL REV 71 AND BOEING DRAWING 147A5810 REV A 2021-12-27
N8607M BOEING 7378H4 During INSP/MAINT - L/H AFT OVERWING EXIT LINER (833AZ) WINDOW REVEAL SUPPORT BROKEN / REMOVED AND REPLACED L/H AFT OVER WING EXIT LINER (833AZ) WINDOW REVEAL SUPPORT IAW DWG # 411A6810-88 AND BAC 5010 PG 73 TYPE 89 A TAG A03666 2021-12-10
N8607M BOEING 7378H4 During INSP/MAINT - C-1 PIT DOOR OPENING THRESHOLD PLATE; AREAS OF CORROSION ON UPPER SIDE OF PLATE; BS440 TO BS480+6; RBL 30; WL 156; AREASMARKED IN BLACK / REMOVED CORROSION FROM FWD CARGO BAY DOOR THRESHOLD PLATE WEB IAW SRM 51-10-02-0G-0 AND INSPECTED W/10X MAG GLASS. VERIFIED MATERIAL LOSS: ORIGINAL T= .036 LOSS = .009' LIMIT = .004' THRESHOLD WEB IS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1 FIG 103 DET D. REMOVED AND REPLACED WEB IAW SRM 51-40-02-0G-0 AND DWG 143A8330 REV:- APPLIEDCIC TO LOWER AND UPPER SURFACES OF WEB IAW AMM 51-21-91-620-802 MPM: 654A0003-58 A-TAG: WN7080 2021-12-07
N8607M BOEING 7378H4 During INSP/MAINT - BS 500I; LBL 24 TO RBL 19; WL 156; C-1 PIT AFT BULKHEAD TO FLOOR ATTACH ANGLE HAS SEVERAL AREAS OF CORROSION AROUND FLOOR BEAM ATTACH FASTENERS ON TOP SIDE OF BEAM; AREAS MARKED IN BLACK / NO ALLOWABLE LIMITS FOUND IN SRM BULK HEAD TO FLOORATTACH ANGLE IS FOUND TO BE OUT OF LIMITS REMOVED AND REPLACED FLOOR ATTACH ANGLE FWD CARGO AFT BULK HEAD STA 500I LBL24 TO RBL 19 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 143A9481 REV - APPLIED CIC TO NEW ANGLE IAW AMM 51-21-91-620-802 MPN 143A9485735 A TAG WN9764 2021-11-18
N8607M BOEING 7378H4 During INSP/MAINT - FORWARD CARGO DOOR AFT LOWER THRESHOLD SCUFF PLATE CRACKED / FORWARD CARGO DOOR AFT LOWER THRESHOLD SCUFF PLATE WAS REPAIRED ON BACKSHOP W/O 41652/1400/0001 SERIAL NO. 7989311 2021-10-07
N8607M BOEING 7378H4 During INSP/MAINT - AFT CARGO DOOR FORWARD CORNER SCUFF PLATE CRACKED / AFT CARGO DOOR FWD CORNER SCUFF PLATE WAS REPAIRED ON BACK SHOP W/O41652/1600/0001 SERIAL NO. 7489314 2021-06-10
N8607M BOEING 7378H4 During INSP/MAINT - LEFT HORIZONTAL STAB FWD SPAR UPPER SLIDING SEAL IS CRACKED AT FWD AND AFT EDGES / REMOVED + REPLACED L/H HORIZONTIAL STAB FWD SPAR UPPER SLIDING SEAL IAW AMM 53-31-31-00-802; SRM 51-40-02-0G-0; + AMM 53-31-31-400-802 A-TAG# A00085 2021-06-10
N8607M BOEING 7378H4 During INSP/MAINT - RIGHT HORIZONTAL STAB FWD SPAR UPPER SLIDING SEAL IS CRACKED AT FWD AND AFT EDGES / REMOVED + REPLACED R/H HORIZONTIAL STAB FWD SPAR UPPER SLIDING SEAL IAW AMM 53-31-31-000-802; SRM 51-40-02-0G-0; + AMM 53-31-31-400-802 ATAG A00091 2021-06-10
N8607M BOEING 7378H4 During INSP/MAINT - WET AREA FLOOR STRUCTURE STA 947.5; LBL 24 INTERCOSTAL UPPER CHORD IS CORRODED. / INTERCOSTAL UPPER CORD CORRODED STA 947.5 BLENDED AND REMOVED CORROSION 'OUT OF LIMITS' OVER 50% LOSS IAW SRM 51-10-02-0G-0 LOCATED AND DRILLED NEW -7 UPPER CORD IAW SRM 51-40-05-0G-0 ALSO BOEING DWG 147A5400 REV - ALODINED AND PRIMED NEW -7 UPPER CORD IAW AMM 51-21-41-370-803AND AMM 51-21-72-370-801 INSTALLED NEW UPPER CORD IAW SRM 51-40-02-0G-0 ALSO BOEING DWG 147A5400 REV - PN 147A5430-7 2021-06-10
N8607M BOEING 7378H4 During INSP/MAINT - AFT CARGO COMPARTMENT; DOOR SILL SUPPORT STRUCTURE; CORRODED; BS792-849; RBL25-35; WL156 / AFT CARGO COMPARTMENT DOOR SILL SUPPORT STRUCTURE CORRODED BS 792-849 RBL 25-35 WL 156 REMOVED DAMAGE IAW SRM 51-10-02-0G-0 FOUND TO BE OUT OF LIMITSORIGINAL T = .050' REMAINING T .031' LOSS OF .019' IAW SRM 53-60-15-1A-1 REMOVED STRUCTURE / WEB IAW SRM 51-40-02-0G-0VERIFIED NEW MATERIAL IAW BOEING DWG # 146A8120 REV A LOCATED & DRILLED AND INSTALLED NUT PLATES ON NEW WEB IAW BOEING DWG # 146A8120 AND SRM 51-40-05 INSTALLED SILL SUPPORT STRUCTURE IAW BOEING DWG # 146A8120 REV A P/N 146A8123-25 A TAG #WN8886 2021-06-10
N8607M BOEING 7378H4 During INSP/MAINT - AFT CARGO COMPARTMENT FLOOR STRUCTURE STA 767 TO 792; RBL 25; WL 154 SHIELD UPPER AND LOWER SURFACE HAS CORROSION. / REMOVED CORROSION AT AFT ACRGO COMPARTMENT FLOOR STRUCTURE STA 767 TO 792 RBL 25 WL 154 SHIELD UPPER AND LOWER SURFACE LOSS.007 ORIG .050 REMAINING .043 OUT OF LIMITS I/A/W SRM 53-60-15-1A-1; REMOVED AND INSTALLED NEW FLOOR SHIELD AT STA 767TO 792 I/A/W SRM 51-40-02-0G-0 AND BOEING DWG# 146A0081 REV:- PN 146A8127-12 ATAG WN9207 2021-06-10
N8607M BOEING 7378H4 During INSP/MAINT - AFT CARGO COMPARTMENT FLOOR STRUCTURE STA 947; RBL 25; WL 179 SIDEWALL SUPPORT ANGLE HAS CORROSION. / REMOVED CORROSIONFROM AFT CARGO COMPARTMENT FLOOR STRUCTURE STA 947; RBL 25 SIDE WALL SUPPORT ANGLE ORIGINAL MATERIAL THICKNESS .080 LOSSOF .001 WITH .079 REMAINING IS OUT OF LIMITS DUE TO NO PUBLISHED LIMITS ACCOMPLISHED AAR EA 200542 REV IR AND SWA W/I NO; NO 20-153-02421 REV IR TO BLEND AND LEAVE AS IS P/N 149A8118-27 2021-06-10
N8607M BOEING 7378H4 During INSP/MAINT - AFT CARGO COMPARTMENT FLOOR STRUCTURE STA 867; LBL 10 BULKHEAD SUPPORT ATTACH CLIP CRACKED. / REMOVED CRACKED AFT CARGOCOMPARTMENT FLOOR STRUCTURE STA 867 LBL 10 BULK HEAD SUPPORT ATTACH CLIP AND REPLACED WITH NEW ATTACH CLIP IAW SRM 51-40-02-0G-0 AND BOEING DWG 149A8102 REV A A TAG A76587 2021-06-10
N8607M BOEING 7378H4 During INSP/MAINT - C-1 PIT; BS500H; LBL 24; WL 156; INTERCOSTAL ATTACH CLIP ON AFT SIDE OF FRAME CRACKED; MARKED IN BLACK / REMOVED AND REPLACED INTERCOSTAL ATTACH CLIP AFT SIDE OF FINAL STA 500H LBL 24 P/N 143A7502-155 TAG#A00731 IAW B737 SRM 51-40-02-0G-0 AND DWG 143A7505- REV.- 2021-06-10
N8607M BOEING 7378H4 During INSP/MAINT - L/H HORIXONTAL STAB FWD UPPER SLIDING SEAL IS CRACKED / R&R LH HORIZONTAL STAB FWD UPPER SLIDDING SEAL PER AMM 53-31-31INSP 44444 2021-06-08
N8607M BOEING 7378H4 During INSP/MAINT - R/H HORIZONTAL STAB FWD UPPER SLIDING SEAL IS CRACKED / R&R RH HORIZONTAL STAB FWD UPPER SLIDDING SEAL PER AMM 53-31-31. 2021-06-08
N8607M BOEING 7378H4 During INSP/MAINT - L2 DOOR Z ANGLE CHORD IS CORROED AT THRESHOLD ATTACH FASTNERS. AFT CARGO COMPARTMENT FLOOR PANEL 140AF FWD EDGE HAS CORROSION. EVALUATED CORROSION; DETERMINED TO BE OUT OF LIMITS (OVER 20') IAW MAM 255200200803 AND SRM 5300531A1 FIG 102. VERIFIED NEW MATERIAL FOR REPLACEMENT. P# 2024T3071 ATAG# A73956. FABRICATED REPLACEMENT PANEL 140AF IAW AMM 255201201801AND BOEING DWG# 453A2610; TREATED IAW AMM 512141370801; PRIMED IAW AMM 512172370804. 2021-05-19
N8607M BOEING 7378H4 During INSP/MAINT - AFT CARGO COMPT. FLOOR PANEL 140AF FWD EDGE HAS CORROSION / AFT CARGO COMPARTMENT FLOOR PANEL 140AF FWD EDGE HAS CORROSION. EVALUATED CORROSION; DETERMINED TO BE OUT OF LIMITS (OVER 20') IAW MAM 25-52-00-200-803 AND SRM 53-00-53-1A-1 FIG 102. VERIFIED NEW MATERIAL FOR REPLACEMENT. P# 2024-T3-071 ATAG# A73956. FABRICATED REPLACEMENT PANEL 140AF IAW AMM 25-52-01-201-801 AND BOEING DWG# 453A2610; TREATED IAW AMM 51-21-41-370-801; PRIMED IAW AMM 51-21-72-370-804. 2021-04-19
N8607M BOEING 7378H4 During INSP/MAINT - FWD CARGO COMPARTMENT FLOOR PANEL120AF AFT EDGE ADJACENT TO THRESHOLD IS CORRODED. / FWD CARGO COMPARTMENT FLOOR PANEL 120AF AFT EDGE ADJACENT TO THRESHOLD IS CORRODED. EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS (OVER 20') IAW SRM 53-00-53-1A-1 FIG 102. VERIFIED NEW MATERIAL; P# 2024-T3-071 ATAG# A36207; + FABRICATED NEW PANEL IAW AMM 25-52-01-201-801 AND BOEING DWG 453A1610. TREATED IAW AMM 51-21-41-370-802; PRIMED IAW AMM 51-21-72-370-804. 2021-04-13
N8607M BOEING 7378H4 During INSP/MAINT - AFT CARGO COMPT. FLOOR PANEL 140CF EDGES HAVE CORROSION / AFT CARGO COMPARTMENT FLOOR PANEL 140CF EDGES HAVE CORROSION EVALUATED CORROSION FOUND TO BE OUT OF LIMITS (OVER 20') IAW SRM 53-00-53-1A-1 FIG 102 REPLACED PANEL VERIFIED NEW MATERIAL (P# 2024-T3-071 A TAG # A73956) IAW AMM 25-52-01-201-801 AND BOEING DWG # 453A2610 FABRICATED NEW PANEL 140CF IAW AMM25-52-01-201-801 AND BOEING DWG # 453A2610 TREATED IAW AMM 51-21-41-370-802 PRIMED IAW AMM 51-21-72-370-804 2021-04-13
N8607M BOEING 7378H4 During INSP/MAINT - BS 500H; RBL 24; WL 153; STR 26R; R/H FLOOR BEAM ZEE ANGLE INTERCOSTAL ATTACH CLIP CRACKED ON FWD SIDE OF FRAME 500H; MARKED IN BLACK / REMOVED AND REPLACED R/H FLOOR BEAM Z ANGLE INTER COSTAL ATTACH CLIP FWD SIDE OF FRAME STA 500H RBL 24 STRINGER 26R P/N 143A7502-158 TAG # A00573 IAW B 737 SRM 51-40-02-0G-0 AND DWG 143A7505 REV - 2021-04-12
N8607M BOEING 7378H4 During INSP/MAINT - BS 500H; RBL 24; WL 153; STR 26R; R/H FLOOR BEAM ZEE ANGLE INTERCOSTAL ATTACH CLIP CRACKED ON AFT SIDE OF FRAME 500H; MARKED IN BLACK / REMOVED AND REPLACED R/H FLOOR BEAM Z ANGLE INTERCOSTAL ATTACH CLIP STA 500H RBL 24 STRINGER 26R P/N 143A7502-154 TAG # A99266 IAW B 737 SRM 51-40-02-0G AND DWG 143A7505 REV - 2021-04-12
N8607M BOEING 7378H4 During INSP/MAINT - BS 500G RBL 24; WL 153; STR 26R; R/H FLOOR BEAM ZEE ANGLE INTERCOSTAL ATTACH CLIP CRACKED ON FWD SIDE OF FRAME 500G; MARKED IN BLACK / REMOVED AND REPLACED R/H FLOOR BEAM Z ANGLE INTERCOSTAL ATTACH CLIP FWD SIDE OF FRAME STA 500G RBL 24 STRINGER 26R P/N 143A7502-158 TAG # A00573 IAW B 737 SRM 51-40-02-0G-0 AND DWG 143A7505 REV - 2021-04-12
N8607M BOEING 7378H4 During INSP/MAINT - BS 500G; RBL 24; WL 153; STR 26R; R/H FLOOR BEAM ZEE ANGLE INTERCOSTAL ATTACH CLIP CRACKED ON AFT SIDE OF FRAME 500G; MARKED IN BLACK / REMOVED AND REPLACED R/H FLOOR BEAM Z ANGLE INTERCOSTAL ATTACH CLIP AFT SIDE OF FRAME STA 500G RBL 24 STRINGER 26R P/N 143A7502-154 TAG # A99268 IAW B 737 SRM 51-40-02-0G AND DWG 143A7505 REV - 2021-04-12
N8607M BOEING 7378H4 During INSP/MAINT - AFT CARGO COMPARTMENT FLOOR STRUCTURE R\H Z ANGLE STA 867 TO 887; RBL 25; WL 170 HAS CORROSION. / REMOVED CORROSION FROMAFT CARGO COMPARTMENT FLOOR STRUCTURE R/H Z ANGLE STA 867 TO 887; RBL 25; WL 170 AND VERIFIED WITH 10X MAGNIFYING GLASSALL CORROSION REMOVED ORIGINAL THICKNESS .040'; REMAINING THICKNESS .035'; MATERIAL LOSS .005' -OUT OF LIMITS IAW SRM 53-00-53-1A-2; FABRICATED NEW R/H Z ANGLE AND INSTALLED IAW BOEING DWGS 146A7502 REV- AND 146A7500 REV - AND SRM 51-00-02-0G-0 146A5702-57 AAR TOOL 36646 DATE 10/07/21 2021-04-12
N8607M BOEING 7378H4 During INSP/MAINT - BS 500H; LBL 24; WL 153; STR 26L; L/H FLOOR BEAM ZEE ANGLE INTERCOSTAL ATTACH CLIP CRACKED ON FWD SIDE OF FRAME 500H; MARKED IN BLACK / REMOVED AND REPLACED L/H FLOOR BEAM & ANGLE INTERCOSTAL ATTACH CLIP P/N 143A7502-159 TAG #A74757 STA 500H LBL 24 STRINGER 26L. IAW B737 SRM 51-40-02-0G-0 AND DWG 143A7505 REV.- 2021-04-12
N8607M BOEING 7378H4 During INSP/MAINT - BS 500H; LBL 24; WL 153; STR 26L; L/H FLOOR BEAM ZEE ANGLE INTERCOSTAL ATTACH CLIP CRACKED ON FWD SIDE OF FRAME 500H; MARKED IN BLACK / REMOVED AND REPLACED L/H FLOOR BEAM & ANGLE INTERCOSTAL ATTACH CLIP P/N 143A7502-159 TAG #A74757 STA 500H LBL 24 STRINGER 26L. IAW B737 SRM 51-40-02-0G-0 AND DWG 143A7505 REV.- 2021-04-12
N8607M BOEING 7378H4 During CRUISE - IAS DISAGREE INDICATION WITH CAPT SIDE AIRSPEED ROLLING BACK AT STABLE CRUISE FL 390. COMPLIED WITH QRC AND BEGAN DECENT. AROUND FL 300 AFTER 10 MINUTES AIRSPEEDS MATCHED AND IAS DISAGREE LIGHT EXTINGUISHED / REMOVED & REPLACED CAPT'S PITOTPROBE PER M/M - REF. 34-11-01.ALSO REMOVED & REPLACED CAPT'S & F.O.'S PER M/M REF. 34-21-04. FOR CAT III UPGRADE SEE FOLLOWING LOGPAGE # 1312761.POS: CAPT TAG: 626353PN/OFF: 0851HT1 S/N OFF: A0293PN/ON: 0851HT1 S/N ON: 232418POS: CG1 TAG:1048572PN/OFF: C17001DA01 S/N OFF: 2665PN/ON: C17001DA01 S/N ON: 12539POS: CG2 TAG: 661988PN/OFF: C17001DA01 S/N OFF: 2698PN/N: C17001CA01 S/N ON: 5350 2021-03-18
N8607M BOEING 7378H4 During CRUISE - IAS DISAGREE INDICATION WITH CAPT SIDE AIRSPEED ROLLING BACK AT STABLE CRUISE FL 390. COMPLIED WITH QRC AND BEGAN DECENT. AROUND FL 300 AFTER 10 MINUTES AIRSPEEDS MATCHED AND IAS DISAGREE LIGHT EXTINGUISHED / REMOVED & REPLACED CAPT'S PITOTPROBE PER M/M - REF. 34-11-01.ALSO REMOVED & REPLACED CAPT'S & F.O.'S PER M/M REF. 34-21-04. FOR CAT III UPGRADE SEE FOLLOWING LOGPAGE # 1312761.POS: CAPT TAG: 626353PN/OFF: 0851HT1 S/N OFF: A0293PN/ON: 0851HT1 S/N ON: 232418POS: CG1 TAG:1048572PN/OFF: C17001DA01 S/N OFF: 2665PN/ON: C17001DA01 S/N ON: 12539POS: CG2 TAG: 661988PN/OFF: C17001DA01 S/N OFF: 2698PN/N: C17001CA01 S/N ON: 5350 2021-03-18
N8607M BOEING 7378H4 During CRUISE - IAS DISAGREE INDICATION WITH CAPT SIDE AIRSPEED ROLLING BACK AT STABLE CRUISE FL 390. COMPLIED WITH QRC AND BEGAN DECENT. AROUND FL 300 AFTER 10 MINUTES AIRSPEEDS MATCHED AND IAS DISAGREE LIGHT EXTINGUISHED / REMOVED & REPLACED CAPT'S PITOTPROBE PER M/M - REF. 34-11-01.ALSO REMOVED & REPLACED CAPT'S & F.O.'S PER M/M REF. 34-21-04. FOR CAT III UPGRADE SEE FOLLOWING LOGPAGE # 1312761.POS: CAPT TAG: 626353PN/OFF: 0851HT1 S/N OFF: A0293PN/ON: 0851HT1 S/N ON: 232418POS: CG1 TAG:1048572PN/OFF: C17001DA01 S/N OFF: 2665PN/ON: C17001DA01 S/N ON: 12539POS: CG2 TAG: 661988PN/OFF: C17001DA01 S/N OFF: 2698PN/N: C17001CA01 S/N ON: 5350 2021-03-18
N8607M BOEING 7378H4 During CRUISE - IAS DISAGREE LT BOTH SIDES. CAPT LOST HIS AIRSPEED AND ALT INDICATIONS. SINGLE CHANNEL SPEED TRIM FAIL BOTH ENGINES WENT IN TO ALT MODE. PERFORMED DFCS BITE TEST FOUND FAULT CODE 34-21038; AIR & GRD LOGIC INVALID. PER FIM 34-21 TASK 824 PSEU BITE TEST AND ADIRS BITE FOUND NR 1 ADIRS INVALID FAULT. R & R LT ADIRS PER AMM 34-21-01 OPS CHECKED GOOD. AIRCRAFTRECERTIFIED TO CAT III STATUS PER MT 734-00-03 VERIFICATION 21097. PART VERIFIED ISSUE 3178471 PN OFF ON HG2050AC11 SNOFF 56004294 SN ON 56015220. 2021-03-08
N8607M BOEING 7378H4 During INSP/MAINT - LEFT MAIN WHEEL WELL STA 663 LOWER BULKHEAD VAPOR BARRIER CRACKED LBL 33 AND 7' UP FROM LOWER WHEEL WELL FAIRING. EVALUATED LT STA 663 VAPOR BARRIER AND FOUND CRACK OF 15' AT LBL 33 FOUND TO BE REPAIRABLE, IAW SRM 57-10-10-2R-2. REPAIREDLT VAPOR BARRIER, IAW SRM 51-70-04 REPAIR 10. RESTORED FINISH IN REPAIR AREA, IAW AMM 51-21-73-370-804 AND AMM 51-71-72-370-804. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - BS 500H; LBL 24; WL 153; STR 26L STRINGER CLIP CRACKED AT FRAME ATTACH RIVETS ON FWD SIDE OF BS 500H FRAME. REMOVED ANDREPLACED STRINGER CLIP AT STA 500H LBL 24 STRINGER 26L P/N 143A1010-28 TAG NR A99263, IAW B 737 SRM 51-40-02-0G-0 AND DWG 143A1233 REV. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - BS 500I; RBL 23; WL 153; STR 26R STRINGER CLIP CRACKED AT CLIP TO FRAME ATTACH RIVET ON FWD SIDE OF FRAME. REMOVED ANDREPLACED STRINGER CLIP AT STA 500I RBL 23 STRINGER 26R P/N 143A1010-48 TAG NR A09840, IAW B 737 SRM 51-40-02-0G-0 AND DWG 143A1234 REV A. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - BS 500I LBL 23 WL 153 STR 26L STRINGER CLIP CRACKED AT CLIP TO FRAME ATTACH RIVETS ON FWD SIDE OF FRAME, MARKED IN BLACK. REMOVED AND REPLACED STRINGER CLIP P/N 143A1010-28 TAG NR A99261 AT STA 500I STRINGER 26L, IAW B737 SRM 51-40-02-0G-0DWG 143A1234 REV A. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - BS 500I; LBL 24; WL 153; STR 26L FLOOR BEAM ZEE ANGLE INTERCOSTAL OUTBOARD ATTACH CLIP CRACKED AT FRAME 500I ATTACH POINT, MARKED IN BLACK. REMOVED AND REPLACED FLOOR BEAM Z-ANGLE INTERCOSTAL OUTBOARD ATTACH CLIP. STA 500I STRINGER 26L LBL 24 P/N 143A7502-165 TAG NR A72795, IAW B737 SRM 51-40-02-0G-0 AND DWG 143A7505 REV. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - C-1 PIT LT SIDEWALL TO FLOOR PANEL ZEE ANGLE HAS AREAS OF CORROSION AROUND SIDEWALL PANEL ATTACH SCREW HOLES FROM BS 500C TO BS 500I, AREAS MARKED IN BLACK. REMOVED CORROSION AT C-1 PIT LT SIDE WALL TO FLOOR PANEL Z ANGLE STA 500C TO 500I,IAW B 737 SRM 51-10-02-0G-0 ITEM 15. ORIGINAL 'T' .040 REMAINING .032 LOSS .008 FOUND TO BE OUT OF LIMITS, IAW B 737 SRM 53-00-53-1A-2 FIG 103. CUT OUT DAMAGE SECTION AT BETWEEN STA 500B AND 500C AND FABRICATED REPAIR SECTION AND SPLICEINSTALLED, IAW B 737 SRM 53-00-53-2A-1 REPAIR 5 P/N 143A7501-187. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - C-1 PIT, RT SIDEWALL TO FLOOR PANEL ZEE ANGLE HAS AREAS OF CORROSION AROUND SIDEWALL PANEL ATTACH SCREW HOLES FROM BS 500A TO BS 500I, AREAS MARKED IN BLACK. REMOVED CORROSION AT C-1 PIT RT SIDE WALL TO FLOOR PANEL Z ANGLE STA 500A TO 500J, IAW B 737 SRM 51-10-02-0G-0 ITEM 15. ORIGINAL 'T' .040 REMAINING .031 LOSS .009 FOUND TO BE OUT OF LIMITS, IAW B 737SRM 53-00-53-1A-2 FIG 103. FABRICATE REPAIR SECTION AND SPLICE INSTALLED, IAW B 737 SRM 53-00-53-2A-1 REPAIR 5 P/N 143A7501-188. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - CABIN FLOOR PANEL 221AF UPPER SURFACE/INSERT DAMAGED. REPAIRED DAMAGED SURFACE AND REPLACED INSERT ON PANEL 221AF, IAWB737-800 SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - CABIN FLOOR PANEL 222AF UPPER SURFACE DAMAGED. REPAIRED CABIN FLOOR PANEL 222AF UPPER SURFACE MISSING FIBERS, IAW B737SRM 53-00-50-2R-1 AND B737 SRM 53-00-50-2R-0 A85487 A72547. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - CABIN FLOOR PANEL 221CF UPPER SURFACE AND INSERTS DAMAGED. REPAIRED AND INSTALLED 3 EA DAMAGED INSERTS ON CABIN FLOOR PANEL 221CF UPPER SURFACE, IAW B737 SRM 53-00-50-2R-1; B737 SRM 53-00-50-2R-0. A72547; A85487; A58925; A21946; A69240. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - CABIN FLOOR PANEL 222BF UPPER SURFACE DAMAGED. REPLACED CABIN FLOOR PANEL 222BF UPPER FIBER DAMAGE, IAW B737-800 SRM 53-00-50-2R-O REPAIR 1 STEPS B1-4; J-P & TABLE 201 TABLE 203 A91653; A72547. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - CABIN FLOOR PANEL 221BF UPPER SURFACE/CORNER DAMAGED. REPAIRED DAMAGED CORNER OF PANEL 221BF, IAW B737-800 SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - CABIN FLOOR PANEL 221DF UPPER SURFACE DAMAGED. REPAIRED CABIN FLOOR PANEL 221DF UPPER SURFACE, IAW B737 SRM 53-00-50-2R-1 AND B737 SRM 53-00-50-2R-1 A33703; A72547. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - CABIN FLOOR PANEL 221FF UPPER SURFACE DAMAGED. REPAIRED CABIN FLOOR PANEL 221FF UPPER SURFACE MISSING FIBERS, IAW B737SRM 53-00-50-2R-1 AND B737 SRM 53-00-50-2R-0 A72547 A85487. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - CABIN FLOOR PANEL 222CF UPPER SURFACE DAMAGED. REPLACED FWD INNER WINDOW PANE AT PASSENGER CABIN SIDEWALL PANEL 241ZAW,IAW AMM 25-21-020-801 AND AMM 25-21-12-400-801 WN8499. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - CABIN FLOOR PANEL 221GF UPPER SURFACE DAMAGED. REPAIRED DAMAGE TO UPPER SURFACE OF FLOOR BOARD 221GF, IAW 737-800 SRM 53-00-50-2R-1 REPAIR 1 REV 71 SRM 53-00-50-2R-0 REPAIR GENERAL REV 71, TAP TEST GOOD. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - CABIN FLOOR PANEL 221EF UPPER SURFACE DAMAGED. REPAIRED AREA OF FRAYED FIBERS ON UPPER SURFACE OF PANEL 221EF, IAW B737-800 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - WET AREA FLOORBOARD 241XF TOP SURFACE PLY IS DAMAGED IN SEVERAL AREAS. REPAIRED AREA OF PULLED FIBERS ON UPPER SURFACEOF PANEL 241XF, IAW B737-800 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - CABIN FLOOR PANEL 222DF UPPER SURFACE DAMAGED. REPAIRED CABIN FLOOR PANEL 222DF UPPER SURFACE MISSING FIBERS, IAW B737SRM 53-00-50-2R-1 AND B737 SRM 53-00-50-2R-0 A85987; A72547. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - AFT CARGO COMPARTMENT FLOOR TIE DOWN RAIL STA 792; RBL 15; WL 154 HAS CORROSION. REMOVED CORROSION, VERIFIED USING X10MAG GLASS,IAW SRM 51-10-02-0G-0. EVALUATED MATERIAL LOSS AS 100% MATERIAL LOSS OUT OF LIMITS SRM 53-00-53-1A-2. REMOVED AFT CARGO TRACK STA 747+14'-STA 887 RBL 13.84 WL 154, IAW 51-40-02-0G-0. VERIFIED NEW CARGO TRACK AS MON:654A0004 ATAG NR WN9052, IAW DWG 146A7500 REV-. VERFIFIED TRACK SPLICE AS PN BAC1509-10688 7050-776811 ATAG NR A94767, IAW SRM 53-00-53-2R-3 REPAIR 3 TABLE 201 ITEM 2. HFEC & OPEN HOLE INSPECTION, NO DEFECTS NOTED, IAW NDT PT6 51-00-00 P-16. ACCOMPLISHED REPAIR, IAW SRM 53-00-53-2R-3 REPAIR 3 REPAIR 4(A-R) COMPLETE P/N 146A7501-41. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - WET AREA FLOORBOARD 242UF TOP SURFACE PLY IS DAMAGED IS SEVERAL AREAS. REPAIRED DAMAGE TO TOP SURFACE OF FLOOR BOARD 242UF, IAW 737-800 SRM 53-00-50-2R-1 REV 71 AND SRM 53-00-50-2R-0 REPAIR GENERAL REV 71. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - WET AREA FLOOR PANEL 242E TOP SURFACE PLY IS DAMAGED. REPAIRED AREAS OF PULLED FIBERS ON UPPER SURFACE OF PANEL 242E, IAW B737-800 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - AFT CARGO COMPARTMENT FLOOR STRUCTURE RT Z-ANGLE STA 727G+10 TO 767; RBL25; WL154 HAS AREAS OF CORROSION. REMOVED CORROSION ON RT Z-ANGLE STA 727G-10 TO 767; RBL 25; WL 145 IN AFT PIT CARGO COMPARTMENT AND VERIFIED WITH 10X MAGNIFYING GLASS. ALL CORROSION REMOVED, IAW SRM 51-10-02-0G-0; ORIGINAL THICKNESS .040' REMAINING THICKNESS .033'; MATERIAL LOSS OF .007' OUT OF LIMITS. FABRICATED REPAIR PARTS FOR RT Z ANGLE AND INSTALLED, IAW SRM 53-00-53-2R-5 AND BOEING DWG 146A7500REV - P/N 146A7502-31 AAR TOOL 36646 DATE 10/07/21. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - WET AREA FLOOR PANEL 241E TOP SURFACE PLY IS DAMAGED. REPAIRED AREA OF FRAYED FIBERS ON UPPER SURFACE OF PANEL 241E, IAW B 737-800 SRM 53-00-50-2R-1 SRM 53-00-50-2R-0. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - C-1 PIT BS 500G+17; LBL 24; WL 156 INTERCOSTAL BETWEEN BS 500G AND 500F FRAMES CRACKED AT TOP RADIUS, MARKED IN BLACK.REMOVED AND REPLACED INTERCOSTAL (BUFFLE) BETWEEN STA 300G AND 500F P/N 143A7510-19 TAG NR A00722, IAW B737 SRM 51-40-02-0G-0 AND DWG 143A7505 REV. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - PASSENGER CABIN FLOOR STA 947.5 LBL 24 WL 208 T-CAP FRAME AT AFT INBOARD LAV D MOUNT, UPPER AND LOWER SURFACE/EDGE IS CORRODED. REMOVED CORROSION PASSENGER CABIN FLOOR STA 947.5 T CAP LBL 24. EVALUATED MATERIAL LOSS & FOUND ORIG 'T' .180REMAINING .100 LOSS OF .080', OUT OF LIMITS. CUT & REMOVED DAMAGED SECTION OF T-CAP. FABRICATED & INSTALLED REPAIR PARTS. REAPPLIED FINISHES, IAW SRM 51-10-02-0G-0; 53-70-51-1A-1; 53-70-51-2R05 REPAIR 5 P/N 147A5504-29. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - PASSENGER CABIN FLOOR STA 947.5 + 2 LBL 24 WL 208 INTERCOSTAL UPPER SURFACE IS CORRODED. REMOVED CORROSION PASSENGER CABIN FLOOR STA 947.5+2 LBL 24 INTERCOSTAL. EVALUATED MATERIAL LOSS & FOUND ORIG 'T' .142 REMAINING .097' LOSS OF .045' OUT OF LIMITS. REMOVED & REPLACED INTERC,OSTAL IAW SRM 51-40-02-0G-0; 51-40-02-0G-0; DWG 147A5650 SHT 13 REV- P/N147A 5560-3. 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - PASSENGER CABIN RT AFT EMERGENCY EXIT LOWER EXIT SIGN LENS BROKEN. REPLACED PASSENGER CABIN RT AFT EMERGENCY EXIT LOWEREXIT SIGN LENS, IAW AMM 33-51-01-960-802 STEP 3C (10). 2021-01-19
N8607M BOEING 7378H4 During INSP/MAINT - FWD LAV A EXTERIOR LIGHT ASSEMBLY CRACKED 448318. REPLACED FWD LAV EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONS CHECK GOOD, IAW AMM 33-51-14-960-802 WN9219. 2021-01-15
N8607M BOEING 7378H4 During INSP/MAINT - LT MLG WHEEL WELL BULKHEAD VAPOR BARRIER CRACKED 14 INCHES LONG STARTING AT LBL 30, 3 IN FROM TOP TO LBL 34. PERFORMEDINTERIM REPAIR TO LT MLG WHEEL WELL FWD BULKHEAD VAPOR BARRIER CRACK, PER SRM 57-10-10-1A-2 & 20-157-00471. PERFORM INSPECTION OF REPAIR AREA AT 1200 FLT CYCLE INTERVALS OR MORE FREQUENTLY. IF CRACK HAS GROWN PAST THE INTERIM SEAL, REF TO PARAGRAPH 4. ALLOWABLE DAMAGE 2 FOR ALLOWABLE DAMAGE LIMITS. REPETITIVE ACTION REQUIRED: PERFORM INSPECTION OF REPAIR AREA AT 1200 FLT CYCLES INTERVALS OR MORE FREQUENTLY. IF CRACK HAS GROWN PAST THE INTERIM REPAIR, REF TO PARAGRAPH 4.ALLOWABLE DAMAGE 2 FOR ALLOWABLE LIMITS. 2020-11-18
N8607M BOEING 7378H4 During INSP/MAINT - LT MLG W/W BULKHEAD VAPOR BARRIER CRACKED 14 INCHES LONG STARTING AT LBL 30 3 IN FROM TOP TO LBL 34 / PERFORMED INTERIMREPAIR TO LT MLG WW FWD BULKHEAD VAPOR BARRIER CRACK PER SRM 57-10-10-1A-2 & 20-157-00471. PERFORM INSPECTION OF REPAIRAREA AT 1200 FLT CYCLE INTERVALS OR MORE FREQUENTLY. IF CARCK HAS GROWN PAST THE INTERIM SEAL. REF. TO PARAGRAPH 4/ALLOWABLE DAMAGE 2 FOR ALLOWABLE DAMAGE LIMITS. 2020-05-15
N8607M BOEING 7378H4 During INSP/MAINT - BATTERY PACK FOR LEFT AFT EMER LIGHTS INOP / REMOVED & REPLACED LEFT AFT EMER LIGHT BATTERY PACK IAW AMM 33-51-06 2020-05-08
N8607M BOEING 7378H4 During NOT REPORTED - AFT EMERGENCY LIGHTS INOPERATIVE. / R&R BATTERY PACK IAW AMM. 2020-04-28
N8607M BOEING 7378H4 During NOT REPORTED - FORWARD EMERGENCY LIGHTS INOPERATIVE. / R&R BATTERY IAW AMM. 2020-04-28
N8607M BOEING 7378H4 During INSP/MAINT - COCKPIT EMERGENCY EXIT LIGHT IN DOME IS VERY DIM RELAMPED COCKPIT EMERGENCY EXIT LIGHT PER AMM 33-14-00. 2020-04-06
N8607M BOEING 7378H4 During UNKNOWN - R2 DOOR SLIDE COVER LOOSE. TIGHTENED COVER PER SIP. 2019-12-31
N8607M BOEING 7378H4 During UNKNOWN - R2 DOOR SLIDE BEZEL AFT LANYARD OFF. SECURED LANYARD PER MM. 2019-09-26
N8607M BOEING 7378H4 During UNKNOWN - LT EMERGENCY AISLE LIGHT LENS MISSING AT ROW 8. R&R LENS ASSEMBLY PER SIP. 2019-04-03
N8607M BOEING 7378H4 During INSP/MAINT - PASSENGER CABIN EMERGENCY LIGHTS LENS CRACKED. R&R LENS IAW MM. 2019-03-26
N8607M BOEING 7378H4 During UNKNOWN - RT OVERHEAD BIN EGRESS LIGHT COVER MISSING BETWEEN ROW 17 TO ROW 18. INSTALLED LIGHT LENS IAW AMM. 2019-03-13
N8607M BOEING 7378H4 During UNKNOWN - L1 DOOR EMERGENCY SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT. 2018-05-21
N8607M BOEING 7378H4 During NOT REPORTED - CENTER AISLE EXIT SIGN COVER FELL OFF. INSTALLED THE SIGN COVER IAW AMM. 2018-01-04
N8607M BOEING 7378H4 During NOT REPORTED - R1 DOOR EMERGENCY EXIT SIGN COVER FELL OFF. INSTALLED THE COVER IAW SIP. 2017-12-26
N8607M BOEING 7378H4 During UNKNOWN - MID CABIN OVERHEAD EMERGENCY EXIT SIGN DAMAGED. R&R SIGN IAW MM. 2017-10-30
N8607M BOEING 7378H4 During INSP/MAINT - EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R & R THE BATTERY PACK IAW AMM. 2017-09-27
N8607M BOEING 7378H4 During INSP/MAINT - EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R & R THE BATTERY PACK IAW AMM. 2017-09-27
N8607M BOEING 7378H4 During INSP/MAINT - EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R & R THE BATTERY PACK IAW AMM. 2017-09-27
N8607M BOEING 7378H4 During UNKNOWN - R1 DOOR LOWER "EXIT" SIGN BROKEN. R&R LENS IAW AMM. 2017-09-27
N8607M BOEING 7378H4 During UNKNOWN - OVERHEAD EMERGENCY LIGHT LENS COVER MISSING AT ROW 10. INSTALLED LENS PER AMM. 2017-08-30
N8607M BOEING 7378H4 During UNKNOWN - RT AISLE EMERGENCY LIGHT LENS MISSING AT ROW 10. INSTALLED LENS PER MM. 2017-07-26
N8607M BOEING 7378H4 During UNKNOWN - CENTER AISLE EXIT SIGN LENS COVER FELL OFF. REINSTALLED COVER PER SIP. 2017-05-19
N8607M BOEING 7378H4 During UNKNOWN - MID CABIN EXIT SIGN LENS LOOSE. SECURED LENS PER SIP. 2017-05-09
N8607M BOEING 7378H4 During INSP/MAINT - R1 DOOR EXIT SIGN BROKEN. R & R THE SIGN IAW MM. 2017-02-03
N8607M BOEING 7378H4 During UNKNOWN - RT EMERGENCY EXIT LIGHT LENS COVER CRACKED AT ROW 10. R&R COVER PER SIP. 2017-01-27
N8607M BOEING 7378H4 During UNKNOWN - LT EMERGENCY EXIT LIGHT LENS COVER CRACKED AT ROW 23. R&R COVER PER SIP. 2017-01-27
N8607M BOEING 7378H4 During NOT REPORTED - R2 DOOR EMERGENCY EXIT LIGHT DAMAGED. R & R THE LIGHT ASSEMBLY IAW SIP. 2016-08-23
N8607M BOEING 7378H4 During INSP/MAINT - EXIT LIGHT LENS LOOSE AT R1 DOOR. R & R LIGHT ASSY IAW MM. 2016-08-02
N8607M BOEING 7378H4 During UNKNOWN - LEFT EMER LIGHT LENS COVER MISSING AT ROW 12. R & R LENS IAW MM. 2016-05-09
N8607M BOEING 7378H4 During UNKNOWN - RIGHT EMER EGRESS BULLNOSE LIGHT LOOSE AT ROW 22. SECURED LIGHT ASSEMBLY IAW SIP. 2016-04-26
N8607M BOEING 7378H4 During UNKNOWN - OVERHEAD CABIN EMER EXIT LIGHT COVER LEN MISSING. INSTALLED LENS IAW MM. 2015-02-24
N8607M BOEING 7378H4 During UNKNOWN - AFT EXIT ROW EMER EXIT SIGN COVER FELL OFF. INSTALLED COVER IAW AMM. 2014-09-24
N8607M BOEING 7378H4 During UNKNOWN - RIGHT OVERHEAD BIN EMER LIGHT LENS CRACKED AT ROW 21. R & R LIGHT ASSEMBLY IAW AMM. 2014-08-05
N8607M BOEING 7378H4 During UNKNOWN - L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. R & R LIGHT ASSEMBLY IAW MM. 2014-07-15
N8607M BOEING 7378H4 During UNKNOWN - CENTER CABIN EMERGENCY EXIT LENS LOOSE. REINSTALLED LENS IAW SIP & MM. 2014-05-29
N8607M BOEING 7378H4 During UNKNOWN - R2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R&R LENS ASSEMBLY IAW MM. 2013-11-04
N8607M BOEING 7378H4 During UNKNOWN - FWD SERVICE DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R & R LIGHT ASSY IAW MM. 2013-09-25

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Explore the Full Dataset

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.