Aircraft Report for n8633a



Registration History for n8633a





N-Number Make Model Serial Location Description Time
N8633A BOEING 737-8H4 36905 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2014-06-02, expiration date 2023-06-30, serial number 36905. 2020-02-04
N8633A BOEING 737-8H4 36905 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2014-06-02, expiration date 2020-06-30, serial number 36905. 2017-02-07
N8633A BOEING 737-8H4 36905 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2014-06-02, expiration date 2017-06-30, serial number 36905. 2014-06-26
N8633A BOEING 737-8H4 36905 DALLAS, TX Aircraft registered to SOUTHWEST AIRLINES CO, airworthiness date 2014-06-02, expiration date 2017-06-30, serial number 36905. 2014-06-26

Service Difficulty Reports for n8633a













































































N-Number Make Model Serial Description Time
N8633A BOEING 7378H4 During INSP/MAINT - L1 DOOR SLIDE LIGHT; OVHD EXIT LIGHT AND LWR EXIT EGRESS LIGHTS INOP. / [01] R/R FAULTY BATTERY CHARGER M1675 REF AMM 33-51-06. OPS CHK SATISFACTORY. 2022-10-13
N8633A BOEING 7378H4 During INSP/MAINT - BATTERY PACK (M2816) FOR R1 DOOR OVHD EMERGENCY EXIT SIGN AND R1 DOOR SLIDE LIGHT WON'T IS DEAD. (WON'T CHARGE) / [01] R&R BATTERY PACK PER AMM 33-51-06. 2022-10-13
N8633A BOEING 7378H4 During TAXI/GRND HDL - EMERGENCY EXIT SIGN COVER MID CABIN DETACHED / [01] REMOVED AND REPLACED MID CABIN EMER EXIT SIGN ASSEMBLY PER AMM 33-51-01 OPS CHECK GOOD 2022-10-06
N8633A BOEING 7378H4 During INSP/MAINT - RH FWD ASILE ABOVE OVERHEAD BIN EMERGENCY LIGHTS INOP BETWEEN ROWS 2-16 RIGHT SIDE / [01] OK TO CONTINUE PER MEL 33-15-02. 2022-09-23
N8633A BOEING 7378H4 During EXTERNAL LOAD - F/A PRIOR TO PUSHBACK INFORMED US OF PULL HANDLE HANGING OUT ON FWD SVC DOOR EMER SLIDE / [01] INSOECTED NORMALM CONDITION OF FWD SVC DOOR SLIDE PER AMM 25-66-01. TUCKED IN HANDLE AS REQUIRED. NO FURTHER ACTION REQUIRED 2022-07-14
N8633A BOEING 7378H4 During INSP/MAINT - CRACK ON AFT CARGO BAY TRACK AT LBL 17 BS 727I. / [01] VERIFIED APPLICABILITY OF SRM 53-00-53-1A-2. CRACK ON CARGO TRACKWAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.;[14] INSTALLED NEW AFT CARGO BAY TRACK SECTION AND TRACK SPLICES BETWEEN BS 727J +8' AND 727H +14' LBL 17 WL 156 IAW SRM 51-40-02-0G-0; SRM 53-00-53-2R-3 REPAIR 3 ALT. 1. PARG 4 STEPS (O;P AND R) AND DWG 146A7500;[15] VERIFIED CORRECTIVE ACTION #14 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - FLOORPANEL 221BF HAS BROKEN TAB AFT OUTBD EDGE. IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 2 TABLE 2.FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F.DAMAGE WILL BE REPAIRED IAW SRM 53-00-50-2R-1.<BR>REMOVED1EA THROUGH INSERT TO FACILITATE REPAIR IAW SRM 53-00-50-2R-1 PARA 3B.REMOVED DAMAGED PLIES ON TANG AREA AND CLEANED IAW SRM 53-00-50-2R-1 PARA 3C-E. INSTALLED REPAIR PLIES USING BMS 8-201TY4 LOT#1486957-3; VACUUM BAGGED; LEAK CHECK GOOD.5X5 LEAK CHECK PASSED PER SRM 53-00-50-2R-1. CURED REPAIR PLIES; UNBAGGED AND TRIMMED EXCESS MATERIAL INSTALLED 1EA PREVIOUSLY REMOVED INSERT USING BMS 5-107 LOT#AK0KP9324K IAW SRM 53-00-50-2R-1 PARA 3M;N. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 727C+13; BS 727C+16. EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727C+13' REMOVED 0.020' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BEOUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED DAMAGED SECTION OF FLOOR TO SIDEWALL SUPPORT AT BS 727-727E + 11'' LBL 21WL 156; FABRICATED; LOCATED AND DRILLED NEW SECTION AND SPLICE REPAIR; SPLICE REPAIR AT BTW BS727E AND 727F; LBL21 AND WL 156 IAW SRM 53-00-53-2R-5. INSTALLED REPAIR PARTS AND FLOOR TO SIDEWALL SUPPORT; INSTALLED BONDING NUTPLATES FROM 727TO 727F PER SRM 51-40-10-2R-0 AND DWG 146A7500. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727F+13; BS 727H+6; BS 727J+10; BS 727J+14; BS 727J+18; BS 747+6; BS 747+14; BS 747+18. /EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727F+13 REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023; VERIFIED CORRECTIVE ACTION STEP 1.; REMOVED DAMAGED FLOOR TO SIDEWALL SUPPORT;LOCATED AND DRILLEDNEW FLOOR TO SIDEWALL SUPPORT AT BS 727-767; RBL 21 WL 156 IAW SRM 51-40-02-0G-0;51-40-05-0G-0 AND DWG 146A7500.; INSTALLED NEW FLOOR TO SIDEWALL SUPPORT AT BS 727-767; RBL 21 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 146A7500;146A0061. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727D+5; BS 727D+6; BS 727D+12. / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727D+6 REMOVED 0.010' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.040' FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING ATS TOOL ID ATS2678 EXP 4/2023. SIDEWALL SUPPORT WILL BE REMOVED AND REPLACED ON FAULT TTG8Q00C9MUW;[02] VERIFIED. TASK COMPLETE. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 22 BS 767+4; BS 767+12. / [01] CORROSION ON SHIELD WAS FOUND TO BE OUTOF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED DAMAGED SHIELD; LOCATED AND DRILLED NEW SHIELD AT BS 767-787 RBL22 WL 158 IAW SRM 51-40-02-0G-0;51-40-05-0G-0 AND DWG 146A0081.;[04] OK TOINSTALL.;[05] OK TO INSTALL GIVEN.;[06] INSTALLED NEW SHIELD AT BS 767-787 RBL22 WL 158 IAW SRM 51-40-02-0G-0 AND DWG 146A0081.;[07] VERIFIED CORRECTIVE ACTION 6. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CORROSION ON AFT CARGO BAY THRESHOLD AT RBL 26 BS 787+8; BS 787+17; BS 807+3; BS 807+14; BS 807+19; BS 827+4; BS 827+11.EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 787+17' REMOVED 0.015' IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.045' FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1 USING ATS TOOL ID ATS2678 EXP 4/2023; VERIFIED CORRECTIVE ACTION STEP 1. REMOVED SUB THRESHOLD WEB PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW THRESHOLD WEB BS 792TO 847 RBL 26 PER SRM 51-40-05-0G-0 AND DWG 146A8340. OK TO INSTALL INSTALLED NEW THRESHOLD WEB BS 792 TO 847 RBL 26 PER SRM 51-40-02-0G-0 AND DWG 146A8340. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CORROSION ON FSD THRESHOLD SUPPORT ANGLE BS312+14 RBL 5 WL 209 .VERIFIED EFFECTIVITY OF SRM 53-10-15-0I-2 FOR STRUCTUREID AND SRM 53-10-15-1A-2 FOR ALLOWABLE DAMAGE.; UPON FURTHER INVESTIGATION FOUND DAMAGE TO BE LOCATED AT BS 312+14; RBL57; WL 209. REMOVED FSD THRESHOLD SUPPORT ANGLE PER SRM 51-40-02.;LOCATED AND DRILLED NEW FSD THRESHOLD SUPPORT ANGLE PER SRM 51-40-05 AND DWG#141A8310. AND REQUEST OK TO INSTALL.;THE FSD THRESHOLD ANGLE.;INSTALLED NEW FSD THRESHOLD ANGLE PER SRM 51-40-02 AND DWG#141A8310.. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - FWD ENTRY DOOR MOPSILL CRACKED ON VERTICAL FLANGE AT BS 302; LBL 56; WL 208.5. / [01] VERIFIED APPLICABILITY OF SRM 53-10-15-1A-1 FOR ALLOWABLE DAMAGE.;[02] EVALUATED DAMAGE ON FWD ENTRY DOOR MOPSILL AT BS 302; LBL 56; WL 208.5. LENGTH OF CRACK FOUND TO BE 0.5'; DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-15-1A-1.;[03] VERIFIED CORRECTIVE ACTION 2;[04] REMOVED FED MOPSILL PER SRM 51-40-02.;[05] LOCATED AND DRILLED NEW FED MOPSILL PER DWG#141A8110; SRM 51-40-05; SRM 51-40-08. AND REQUEST OK TO INSTALL.;[06] VERIFIED CORRECTIVE ACTION 5- OK TO INSTALL MOP SILL.;[07] INSTALLED NEW FWD ENTRY DOOR MOPSILL PER SRM 51-40-02-0G-0 AND BOEING DWG 141A8110.;[08] VERIFIED CORRECTIVE ACTION #7 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CORROSION ON FWD CARGO BAY FWD DOOR SHIELD AT RBL 25 BS 420+9; BS 420+12. / [01] CORROSION ON SHIELD WAS FOUND TO BE OUTOF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED MEASUREMENT TABLE AND CORRECTIVE ACTION 1.;[03] REMOVEDFWD CARGO BAY FWD DOOR SHIELD AT RBL 25 BS 420- BS 440 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW SHIELD AT RBL25 BS 420- BS 440 PER SRM 51-40-05-0G-0 AND DWG 143A0080.<BR>OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION STEPS 3 AND4. VERIFIED OK TO INSTALL.;[06] INSTALLED NEW SHIELD AT BS 420- BS 440 RBL 25 PER SRM 51-40-02-0G-0 AND DWG 143A0080.;[07] VERIFIED CORRECTIVE ACTION STEP 6.;[08] VERIFIED MEASUREMENT TABLE AND TASK COMPLETE. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH ANGLE AT LBL 25 BS 440+19. / [01] ANGLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED AND REPLACED NEW BAFFLE CLIP T BS 440+19 LBL 25 PER SRM 51-40-02-0G-0 AND DWG 143A7505;[04] VERIFIED CORRECTIVE ACTION #3 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH ANGLE AT RBL 24 BS 500H+1. / [01] ANGLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED AND REPLACED NEW BAFFLE CLIP BS 500H+1 RBL 24 PER SRM 51-40-02-0G AND DWG 143A7505;[04] VERIFIED MEASUREMENTS;[05] VERIFIED CORRECTIVE ACTION #3 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CORROSION ON AFT CARGO BAY AFT DOOR SHIELD AT RBL 21 BS 847+19. / [01] CORROSION ON SHIELD WAS FOUND TO BE OUT OF LIMITSDUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED SHIELD AT BS847- BS867 RBL21 PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW SHIELD AT BS847- BS867 RBL 21 PER SRM 51-40-05-0G-0 AND DWG 146A0081;[05] OK TO INSTALL SHIELD.;[06] OK TO INSTALL GIVEN.;[07] INSTALLED SHIELD AT BS 847- BS867 RBL 21 PER SRM 51-40-02-0G-0 AND DWG 146A0081;[08] VERIFIED CORECTIVE ACTION 7. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH ANGLE AT LBL 25 BS 500H+1. / [01] ANGLE FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED AND REPLACED NEW BAFFLE CLIP BS 500H+1 LBL 25 PER SRM 51-40-02-0G AND DWG 143A7505;[04] VERIFIED MEASUREMENTS;[05] VERIFIED CORRECTIVE ACTION #3 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CRACK ON FWD CARGO BAY GUSSET AT BS 500I R/H STRINGER 19. / [01] CRACKED GUSSET FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED FCB GUSSET AT BS 500I R/H STRINGER 19 PERSRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW GUSSET AT BS 500I R/H STRINGER 19 PER SRM 51-40-05-0G-0 AND DWG 143A7902.<BR>OK TO INSTALL.;[05] VERIFIED CORRECTIVE ACTION 4. OK TO INSTALL.;[06] INSTALLED GUSSET AT BS 500I R/H STRINGER 19 PER SRM 51-40-02-0G-0 AND DWG 143A7902.;[07] VERIFIED CORRECTIVE ACTION 6.;[08] WORKSCOPE COMPLETE. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CORROSION ON FWD CARGO BAY AFT DOOR SHIELD AT RBL 24 BS 500+3; BS 500+7; BS 500+16. / [01] CORROSION ON SHIELD WAS FOUNDTO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED MEASUREMENT TABLE AND CORRECTIVE ACTION 1.;[03] REMOVED FCB CARGO BAY AFT DOOR SHIELD AT RBL 24 BS 492- BS 500A PER SRM 51-40-02-0G-0;[04] LOCATED AND DRILLED NEW SHIELD AT BS 492- BS 500A RBL 24 PER SRM 51-40-05-0G-0 AND DWG 143A0080.<BR>OK TO INSTALL;[05] VERIFIED CORRECTIVE ACTION 4.;[06] INSTALLED SHIELD AT BS 492- BS 500A RBL 24 PER SRM 51-40-02-0G-0 AND DWG 143A0080.;[07] VERIFIED CORRECTIVE ACTION 6.;[08] WORKSCOPE COMPLETE 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CORROSION ON FWD CARGO BAY THRESHOLD AT RBL 24 BS 440+3; RBL 28 BS 460+10; RBL 28 BS 460+13; RBL 28 BS 460+18; RBL 28 BS480; RBL 23 BS 480+10. EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 460+10' REMOVED 0.015'IN A AREA OF 1'X1' ORIGINAL THICKNESS 0.045' FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1. VERIFIED SRM 53-30-15-1A-1IS APPLICABLE. VERIFIED FWD CARGO BAY THRESHOLD WEB CORROSION REWORK IS OUT OF LIMITS PER SRM 53-30-15-1A-1. LOCATED AND DRILLED NEW SUB THRESHOLD WEB BS 440 TO 492 PER SRM 51-40-05-0G-0 AND DWG 143A8330. INSTALLED THRESHOLD WEB ON FWD CARGO BAY BS 440 TO 492 PER SRM 51-40-02-0G-0 AND DWG 143A8330 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - CRACK ON FWD CARGO BAY BAFFLE TO FRAME ATTACH ANGLE AT LBL 25 BS 500H-1' / [01] ANGLE WAS FOUND TO BE OUT OF LIMITS DUETO NO LIMITS ARE GIVEN IN THE SRM.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] REMOVED AND REPLACED NEW BAFFLE CLIP T BS 500H-1 LBL 25 PER SRM 51-40-02-0G-0 AND DWG 143A7505;[04] VERIFIED CORRECTIVE ACTION #3 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - RIGHT AFT GALLEY EMERG. EXIT INDEXER LIGHT IS INOP / [01] AS DOCUMENTED ON CCN: TTG8Q00CLJMN; <BR>REMOVED; REPLACED ANDPERFORMED GOOD INSTALLATION CHECK OF BOTH M1672 BATTERY PACK AND BATTERY CHARGER IAW AMM 33-51-06-960-806 AND AMM 33-51-06-960-805. LIGHTS ASSOCIATED WITH M1672 BATTERY NOW ILLUMINATE PROPERLY.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - RIGHT AFT EMERGENCY LIGHT OVER SERVICE DOOR IS NOT WORKING / [01] AS DOCUMENTED ON CCN: TTG8Q00CLJMN; <BR>REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION CHECK OF BOTH M1672 BATTERY PACK AND BATTERY CHARGER IAW AMM 33-51-06-960-806 AND AMM 33-51-06-960-805. LIGHTS ASSOCIATED WITH M1672 BATTERY NOW ILLUMINATE PROPERLY.;[02] VERIFIED CORRECTIVE ACTION ENTRY1. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - EMERG. EXIT BIN LIGHT AT ROW 10FED IS INOP / [01] REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION TEST OF M1676 BATTERY PACK USING SERVICABLE UNIT IAW AMM 33-51-06-960-805. LIGHTS ASSOCIATED WITH M1676 BATTERY PACK NOW ILLUMINATE PROPERLY.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - EMERG. EXIT BIN LIGHT AT ROW 6-7FED IS INOP / [01] AS DOCUMENTED ON CCN: TTG8Q00CLJMD;<BR>REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION TEST OF M1676 BATTERY PACK USING SERVICABLE UNIT IAW AMM 33-51-06-960-805. LIGHTS ASSOCIATED WITH M1676 BATTERY PACK NOW ILLUMINATE PROPERLY.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - EMERG. EXIT BIN LIGHT AT ROW 25FED IS INOP / [01] AS DOCUMENTED ON CCN: TTG8Q00CLJMN; <BR>REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION CHECK OF BOTH M1672 BATTERY PACK AND BATTERY CHARGER IAW AMM 33-51-06-960-806 AND AMM 33-51-06-960-805. LIGHTS ASSOCIATED WITH M1672 BATTERY NOW ILLUMINATE PROPERLY.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - AFT SERVICE DOOR SLIDE LIGHT IS INOP / [01] REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION CHECK OF BOTH M1672 BATTERY PACK AND BATTERY CHARGER IAW AMM 33-51-06-960-806 AND AMM 33-51-06-960-805. LIGHTS ASSOCIATED WITH M1672 BATTERY NOW ILLUMINATE PROPERLY.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - EMERG. EXIT BIN LIGHT AT ROW 14FED IS INOP / [01] AS DOCUMENTED ON CCN: TTG8Q00CLJMD;<BR>REMOVED; REPLACED AND PERFORMEDGOOD INSTALLATION TEST OF M1676 BATTERY PACK USING SERVICABLE UNIT IAW AMM 33-51-06-960-805. LIGHTS ASSOCIATED WITH M1676 BATTERY PACK NOW ILLUMINATE PROPERLY.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - R/H FWD OVERWING EMERG. EXIT LIGHT INOP / [01] AS DOCUMENTED ON CCN: TTG8Q00CLJMD;<BR>REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION TEST OF M1676 BATTERY PACK USING SERVICABLE UNIT IAW AMM 33-51-06-960-805. LIGHTS ASSOCIATED WITH M1676BATTERY PACK NOW ILLUMINATE PROPERLY.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - RIGHT AFT EMERGENCY LIGHT OVER SERVICE DOOR IS NOT WORKING / [01] AS DOCUMENTED ON CCN: TTG8Q00CLJMN; <BR>REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION CHECK OF BOTH M1672 BATTERY PACK AND BATTERY CHARGER IAW AMM 33-51-06-960-806 AND AMM 33-51-06-960-805. LIGHTS ASSOCIATED WITH M1672 BATTERY NOW ILLUMINATE PROPERLY.;[02] VERIFIED CORRECTIVE ACTION ENTRY1. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - RIGHT AFT GALLEY EMERG. EXIT INDEXER LIGHT IS INOP / [01] AS DOCUMENTED ON CCN: TTG8Q00CLJMN; <BR>REMOVED; REPLACED ANDPERFORMED GOOD INSTALLATION CHECK OF BOTH M1672 BATTERY PACK AND BATTERY CHARGER IAW AMM 33-51-06-960-806 AND AMM 33-51-06-960-805. LIGHTS ASSOCIATED WITH M1672 BATTERY NOW ILLUMINATE PROPERLY.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - EMERG. EXIT BIN LIGHT AT ROW 25FED IS INOP / [01] AS DOCUMENTED ON CCN: TTG8Q00CLJMN; <BR>REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION CHECK OF BOTH M1672 BATTERY PACK AND BATTERY CHARGER IAW AMM 33-51-06-960-806 AND AMM 33-51-06-960-805. LIGHTS ASSOCIATED WITH M1672 BATTERY NOW ILLUMINATE PROPERLY.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. 2022-05-26
N8633A BOEING 7378H4 During INSP/MAINT - AFT SERVICE DOOR SLIDE LIGHT IS INOP / [01] REMOVED; REPLACED AND PERFORMED GOOD INSTALLATION CHECK OF BOTH M1672 BATTERY PACK AND BATTERY CHARGER IAW AMM 33-51-06-960-806 AND AMM 33-51-06-960-805. LIGHTS ASSOCIATED WITH M1672 BATTERY NOW ILLUMINATE PROPERLY.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. 2022-05-26
N8633A BOEING 7378H4 During TAKEOFF - ON T/O ROLL; #2 N1 LAGGED #1 BY 3%. ENGINE WOULD NOT RESPOND TO THROTTLE INPUTS / [01] R/R HMU & FUEL PUMP ON #2 ENG. IAW MT 773-21-10; OPS LK CKS OK;[02] R/R HMU & FUEL PUMP ON #2 ENG IAW MT 773-21-10 ; OPS LK CKS OK 2022-04-27
N8633A BOEING 7378H4 During TAKEOFF - ON T/O ROLL; #2 N1 LAGGED #1 BY 3%. ENGINE WOULD NOT RESPOND TO THROTTLE INPUTS / [01] R/R HMU & FUEL PUMP ON #2 ENG. IAW MT 773-21-10; OPS LK CKS OK;[02] R/R HMU & FUEL PUMP ON #2 ENG IAW MT 773-21-10 ; OPS LK CKS OK 2022-04-27
N8633A BOEING 7378H4 During UNKNOWN - OVERWING EXIT/SALIVA SIGN COVER FELL OFF ; / [01] SECURED OVERWINTER EXIT/SALIDA SIGN COVER PER AMM SIP. 2022-03-04
N8633A BOEING 7378H4 During UNKNOWN - OVERHEAD EXIT LIGHT BROKEN ; / [01] RESECURED OVERHEAD EMERGENCY EXIT LIGHT REF AMM 20-60-11 OPS CHECK GOOD 2022-03-02
N8633A BOEING 7378H4 During INSP/MAINT - CENTER FLOOR SUPPORT AT STA. 540 CRACKED / REMOVED & REPLACED CENTER FLOOR SUPPORT @ STA 540 IAW SRM 51-40-02 (BREAK ASSY PANEL) 2022-02-25
N8633A BOEING 7378H4 During NOT REPORTED - LIGHT HAZE OBSERVED AFT OF OVERWING EXITS AND ELECTRICA SMELL THROUGHOUT CABIN AND COCKPIT ;ACCOMPLISHED QRC AND QRH SMELLAND HAZE DISSAPATED FOLLOWING QRH PROCEDURES / [01] C/W CONDITIONAL INSP IAW M.M 05-51=56; FOUND C/B POPPED ONP-91 PANEL FOR ALT BATT CHARGER; SEE LG PG 194928 2022-02-18
N8633A BOEING 7378H4 During INSP/MAINT - L/H WING T/E PANEL 551FB FWD BRACKET IS BROKEN (MARKED) / REMOVED AND REPLACED L/H WING T/E PANEL 551FB FWD BRACKET IAW737-800 SRM 51-40-02-0G-0 STEP 4. 2022-01-19
N8633A BOEING 7378H4 During INSP/MAINT - ***CORROSION*** R/H FWD THRESHOLD IN AFT CARGO BAY HAS MULTIPLE AREAS OF CORROSION FROM STA 767-787 RBL 22 WL 150 / REMOVED AND REPLACED AFT CARGO SHIELD AT STA 767-787 P/N 146A8127-12 DWG 146A0081 PO 777849 IAW SRM 51-48-02-0G-0 59215U 05MAY20 2021-12-07
N8633A BOEING 7378H4 During INSP/MAINT - ***CORROSION*** R/H AFT THRESHOLD IN AFT CARGO BAY HAS MULTIPLE AREAS OF CORROSION FROM STA 847-867 RBL 22 WL 166 / REMOVED AND REPLACED R/H AFT SHIELD IN CARGO BAY AT STA. 847-867 P/N 146A8127-10 PO# 765476 IN REFERENCE BOEING DWG 146A0081ID 28; 146A8127 ID 7 AND SRM 51-40-02 2021-12-07
N8633A BOEING 7378H4 During INSP/MAINT - BAFFLE CRACKED BETWEEN BS 500C AND 500D R/H STRINGER 26 / REMOVED CRACKED BAFFLE FROM BS 500C-500D R/H STR 26. LOCATED AND DRILLED AND INSTALLED REPLACEMENT BAFFLE BS 500C-500D R/H STR 26 IAW B737-800 SRM 51-40-05 SRM 51-40-02 DWG# 143A7505SHEET 18 REV A. BAFFLE ITEM# 143A7510-24 PO# 792290 2021-11-18
N8633A BOEING 7378H4 During INSP/MAINT - BAFFLE BS 500F TO 500G LBL 25 IS CRACKED / REMOVED FWD CARGO BAFFLE L/H SIDE AT STA 500F-500G IAW SRM 51-40-02-0G-0. INSTALLED BAFFLE REPAIR IAW SRM 53-30-53-2R-1. INSTALLED BAFFLE IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7505 PART# 143A7510-19 P.O.# 792231 LOT# 5088298-1 P.O.# 763260 2021-11-18
N8633A BOEING 7378H4 During INSP/MAINT - AFT GALLEY L/H EMERGENCY LIGHTING INOP / REMOVED & REPLACED BATTERY PACK IAW AMM 33-51-06 2021-08-09
N8633A BOEING 7378H4 During NOT REPORTED - EMERGENCY LIGHT STRIP FORWARD NOT LIGHTING / R/R FWD PHOTO LUMINESCENT STRIP IAW 33-51-15 OPS CHECKED FOUND GOOD 2021-08-02
N8633A BOEING 7378H4 During INSP/MAINT - R2 DOOR LINER LOWER SUPPORT ASSY CRACKED / R&R R2 DOOR LINER LOWER SUPPORT ASSY PER AMM 52-41-31AMT 117477INSP 31326 2021-04-12
N8633A BOEING 7378H4 During CRUISE - AFT F/A JUMPSEAT FLASHLIGHT STRAP BROKEN. REPLACED STRAP ON AFT FLASHLIGHT, IAW SIP. 2020-12-16
N8633A BOEING 7378H4 During INSP/MAINT - AFT GALLEY EMERGENCY EXIT LIGHT COVER MISSING LETTERING. REPLACED COVER, PER MM 33-51-11. 2020-11-12
N8633A BOEING 7378H4 During INSP/MAINT - EMERGENCY LIGHT JUST AFT OF AFT ENTRY DOOR INOPERATIVE. R & R THE LAMP ON EMERGENCY LIGHT IAW MM 33-51-04. 2020-08-06
N8633A BOEING 7378H4 During INSP/MAINT - *CUSTOMER REQUEST* L/H LOWER STA 663 UPPER ATTACH ANGLE IS CRACKED AT LBL9 / REMOVED DAMAGED SECTION OF BS 663 UPPER ATTACH ANGLE AT LBL 6-15 AND REPAIRED PER SRM 57-10-10-2R-5. APPLIED CIC TO REPAIR & CAP SEALED FASTENERS ON VAPOR BARRIERAND IN FUEL TANK PER SRM 57-10-10-2R-5 2020-05-22
N8633A BOEING 7378H4 During INSP/MAINT - *CUSTOMER REQUEST* LOWER STA 663 UPPER ATTACH ANGLE IS CRACKED AT RBL9 / REMOVED DAMAGED SECTION OF BS 663 UPPER ATTACHANGLE AT RBL 6-15 AND REPAIRED PER SRM 57-10-10-2R-5; APPLIED CIC TO REPAIR & CAP SEALED FASTENERS ON VAPOR BARRIER ANDIN FUEL TANK PER SRM 57-10-10-2R-5 2020-05-22
N8633A BOEING 7378H4 During INSP/MAINT - ALL EMERGENCY LIGHTS IN THE FWD GALLEY AREA DO NOT ILLUMINATE. / TROUBLESHOOTING; REMOVE AND REPLACE BATTERY PACK M2816;PERFORMED OPS CK FOR ALL EMERGENCY LIGHTS IN FWD. GALLEY AREA IAW AMM 33-51-06; AND WDM 33-51-12 OPS CK GOOD 2020-05-22
N8633A BOEING 7378H4 During INSP/MAINT - RH SKATE ANGLE VERTICLE FLANGE WORN STA 1120 TO STA 1123 / PERFORMED SRM 53-80-71-2R-6 REPAIR 6 ON R/H SKATE ANGLE FROMSTA 112 TO STA 1132; RESTORED EXTERIOR FINISH PER SRM 53-80-71-2R-6 92385U 05/12/20 2020-05-22
N8633A BOEING 7378H4 During INSP/MAINT - ***CORROSION*** L/H Z-CHANNEL IN FWD CARGO BAY HAS MULTIPLE AREAS OF CORROSION FROM STA 480-500I LBL 25 WL 155 / REMOVEDDAMAGED L/H Z-CHANNEL IN FWD CARGO BAY FROM STA 480-500I LBL 25 WL 155; INSTALLED SPLICE IS AT 480+10 & 500D+10; & REPLACEMENT Z-CHANNEL IAW SRM 53-00-53-2R-5. 2020-05-19
N8633A BOEING 7378H4 During INSP/MAINT - ***CORROSION*** AFT BULKHEAD TO FLOOR SUPPORT IN FWD CARGO BAY HAS MULTIPLE AREAS OF CORROSION AT STA 500I FROM LBL 25-RBL 25 WL 155 / CORROSION FOUND TO BE OUT OF LIMITS ON AFT BULKHEAD FLOOR SUPPORT I.A.W SRM 53-00-53-1A-2 FIG E. REMOVEDBULKHEAD TO FLOOR SUPPORT I.A.W. SRM 51-40-02-0G-0. INSTALLED NEW BULKHEAD TO FLOOR SUPPORT P/O# 778494/1 I.A.W. SRM 51-40-02-0G-0 AND BOEING DWG 143A9481 REV A AND DWG 143A7902 REV:B. 2020-05-19
N8633A BOEING 7378H4 During INSP/MAINT - ***CORROSION*** R/H AFT Z-CHANNEL IN FWD CARGO BAY HAS MULTIPLE AREAS OF CORROSION FROM STA 500-500I RBL 25 WL 155 / CORROSION FOUND ON R/H Z CHANNEL IN FWD CARGO BAY FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 DETAIL D. REMOVED AND REPLACED R/H Z CHANNEL FROM 500-500I; RBL 25; WL 155; ITEM# BAC1496-444; LOT# 5090953-1; PO# 773837/1; P/N 143A7501-188; IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A7500 59321U 5/10/20 2020-05-18
N8633A BOEING 7378H4 During INSP/MAINT - ***CORROSION*** R/H AFT Z-CHANNEL IN AFT CARGO BAY HAS MULTIPLE AREAS OF CORROSION FROM STA 867-947 RBL 22 WL 166 / EVALUATED DAMAGE ON AFT CARGO BAY Z-CHANNEL STA 867 947 RBL 22; FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED Z CHANNEL STA 867-947 RBL 22 IAW SRM 51-40-02-0G-0; AND DRAWING # 147A7501 & 146A7500. 2020-05-18
N8633A BOEING 7378H4 During INSP/MAINT - ***CORROSION*** L/H Z-CHANNEL IN AFT CARGO BAY HAS MULTIPLE AREAS OF CORROSION FROM STA 727+4' TO 847 LBL 22 WL 155 / REMOVED L/H Z-CHANNEL IN AFT CARGO BAY FROM STA 727+4' TO 847 LBL 22 WL 155. REPLACED WITH NEW Z-CHANNEL PO # 786862 IN AFT CARGO L/H STA 727+4' TO 847 LBL 22 WL 155 IAW SRM 51-40-02 AND BOEING DWG # 146A7502. 57828U 5/12/2020 2020-05-18
N8633A BOEING 7378H4 During INSP/MAINT - ***CORROSION*** R/H Z-CHANNEL IN AFT CARGO BAY HAS MULTIPLE AREAS OF CORROSION FROM STA 727F+10' TO 767 RBL 22 WL 155 /R/H Z-CHANNEL IN AFT CARGO BAY HAS CORROSION FROM 727F+10 - 767; RBL 22; WL 155; FOUND TO BE OUT OF LIMITS PER SRM 53-00-01-1A-2; P/N 146A7502-10. REMOVED AND REPLACED R/H Z-CHANNEL STA 727F+10 - 767; RBL 22; WL 155; P/N 146A7502-10; ITEM #BAC1496-377; LOT # 5093799-1; PO # 786416/1 IAW SRM 51-40-02-0G-0 AND SRM 53-00-53-2R-5; AND BOEING DWG 146A7500; SPLICE PLATE LOCATION VERIFIED AT STA 727F+10 2020-05-15
N8633A BOEING 7378H4 During CLIMB - ON INITIAL CLIMB OUT FLIGHT ATTENDANTS REPORTED A SLIGHT ELECTRIC BURNING SMELL THAT LASTED FOR JUST A FEW SECONDS AND THEN STOPPED. THE SMELL CAME FROM THE AFT GALLEY. R&R AFT 2 COFFEE MAKER PER AMM. 2020-01-02
N8633A BOEING 7378H4 During CLIMB - ON INITIAL CLIMB OUT FLIGHT ATTENDANTS REPORTED A SLIGHT ELECTRIC BURNING SMELL THAT LASTED FOR JUST A FEW SECONDS AND THEN STOPPED. THE SMELL CAME FROM THE AFT GALLEY. R&R AFT 1 COFFEE MAKER PER AMM. 2020-01-02
N8633A BOEING 7378H4 During INSP/MAINT - FORWARD RT LUMINESCENT TRACK LIGHTS DAMAGED. R&R LIGHTS PER AMM. 2019-03-08
N8633A BOEING 7378H4 During INSP/MAINT - FORWARD LT LUMINESCENT TRACK LIGHTS DAMAGED. R&R LIGHTS PER AMM. 2019-03-08
N8633A BOEING 7378H4 During INSP/MAINT - AFT LT LUMINESCENT TRACK LIGHTS DAMAGED. R&R LIGHTS PER AMM. 2019-03-08
N8633A BOEING 7378H4 During INSP/MAINT - AFT RT LUMINESCENT TRACK LIGHTS DAMAGED. R&R LIGHTS PER AMM. 2019-03-08
N8633A BOEING 7378H4 During INSP/MAINT - R2 DOOR SLIDE ATTACH SCREW MISSING. INSTALLED A NEW SCREW IAW MM. 2019-01-29
N8633A BOEING 7378H4 During INSP/MAINT - LEFT HORIZONTAL STABILIZER TIP TRAILING EDGE CORNER MISSING. R & R THE TIP CAP ASSEMBLY IAW AMM. 2018-10-24
N8633A BOEING 7378H4 During UNKNOWN - LT OVERWING EMERGENCY EXIT EMERGENCY LOWER LIGHT LENS DETACHED. INSTALLED COVER PER MM. 2018-07-09
N8633A BOEING 7378H4 During UNKNOWN - R2 DOOR EXIT SIGN FELL OFF. R&R LENS BASE ASSEMBLY IAW AMM. 2017-08-22
N8633A BOEING 7378H4 During UNKNOWN - R1 DOOR PLASTIC "EXIT" COVER LENS MISSING. INSTALLED LENS PER M/M. 2016-12-23
N8633A BOEING 7378H4 During UNKNOWN - R1 DOOR LOWER EMER EXIT SIGN MISSING. R & R SIGN ASSEMBLY IAW SIP. 2015-08-25
N8633A BOEING 7378H4 During UNKNOWN - LEFT EMER EXIT BULLNOSE LIGHT LENS COVER MISSING AT ROW 12. INSTALLED LENS IAW MM. 2015-03-02
N8633A BOEING 7378H4 During UNKNOWN - R1 DOOR LIGHTED EXIT LIGHT COVER LENS LOOSE. SECURED LENS IAW MM. 2014-09-18

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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.