# Boeing 737-25A - Type: Aircraft model (FAA registry) - Registry code: 1384481 - Manufacturer (registry): BOEING - Model: 737-25A - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-fan - Seats: 130 - Weight class: 20,000 lb and over - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/boeing-737-25a Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft None registered with this model now. ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (161, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR TSAA0524018](https://openairdocs.org/sdr/TSAA0524018), Apr 4, 2005: CIRCUIT BREAKER. DAMAGED. CREW REPORTED SMOKE IN THE COCKPIT. SMOKE FROM CB PANEL BEHIND F/O. SLIDING WINDOW OPENED TO VENT SMOKE. RETURNED TO GATE. REMOVED AND REPLACED THE APU GCU. DID - [SDR TSAA0421081](https://openairdocs.org/sdr/TSAA0421081), Nov 30, 2004: CLAMP. LOOSE. PRESSURIZATION CHECKED BEFORE TAKEOFF, CABIN CLIMBED TO 1,000 FT BY THE TIME AIRCRAFT LEVELED AT 3,000 FT. RETURNED TO OGG. NOTE THAT THE RIGHT PACK WAS DEACTIV - [SDR TSAA0472079](https://openairdocs.org/sdr/TSAA0472079), Nov 27, 2004: ENGINE. FAILED. NON-ETOPS FLT. 241, HNL-LIH: CLIMBING THROUGH 8,000 FEET, HEARD A LOUD BANG AND THE AIRCRAFT YAWED RIGHT. THE NR 2 ENGINE EPR DROPPED FROM 1.82 TO 1.76. REPORTE - [SDR TSAA0473068](https://openairdocs.org/sdr/TSAA0473068), Sep 14, 2004: FCU. MALFUNCTIONED. ON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, ENGINE POWER ADVANCED NORMALLY UNTIL 1.96-1.97 EPR INDICATION. MAX-POWER OBTAINED WAS 1.97 EPR WITH N1 AT - [SDR TSAA0431067](https://openairdocs.org/sdr/TSAA0431067), Sep 12, 2004: INDICATOR. SLOW. NON-ETOPS FLIGHT 62, HNL-OGG: ON TAKEOFF 80KTS CROSS-CHECK WAS OK, AFTER LIFTOFF THE FIRST-OFFICERS AIRSPEED INDICATOR READ 50KTS SLOWER THAN CAPTAIN’S STANDBY - [SDR TSAA0477066](https://openairdocs.org/sdr/TSAA0477066), Sep 11, 2004: ENGINE. MALFUNCTIONED. ON TAKEOFF UNABLE TO OBTAIN MAX-POWER ON NR 1 ENGINE, MAX-EPR INDICATION OF 1.96. RETURNED TO HNL. CLEANED DEBRIS FROM PT2 LINE AND VERIFIED SECURITY OF ALL EPR - [SDR RYN2004F00019](https://openairdocs.org/sdr/RYN2004F00019), May 3, 2004: DOUBLER. TORN. AT C-CHECK, FOUND TEAR IN R-1 DOOR THRESHOLD DOUBLER, AT STATION 392. - [SDR TSAA0452026](https://openairdocs.org/sdr/TSAA0452026), Feb 4, 2004: DOOR FRAME. CORRODED. FOUND CORROSION ON FORWARD CARGO DOOR FRAME. TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED REPAIR DOUBLERS AND TRIPLER. ALODINED AND PRIMED - [SDR TSAA0477018](https://openairdocs.org/sdr/TSAA0477018), Jan 9, 2004: CIRCUIT BREAKER. TRIPPED. FLT 280 - HNL-KOA - ABORTED TAKEOFF DUE TO BOTH EPR GAUGES INOPERATIVE. C/B'S RESET, NO FLAGS. RAN BOTH NR 1 AND NR 2 ENGINE AFTER EPR C/B RESET. OPS CHECK GOOD - [SDR TSAA0333147](https://openairdocs.org/sdr/TSAA0333147), Jun 7, 2003: BATTERY PACK. INOPERATIVE. REPLACED AFT ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0333146](https://openairdocs.org/sdr/TSAA0333146), Jun 7, 2003: BATTERY PACK. INOPERATIVE. REPLACED FORWARD ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO LOW VOLTAGE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0353150](https://openairdocs.org/sdr/TSAA0353150), May 22, 2003: CREASE BEAM. CORRODED. FOUND CORROSION DISCOVERED ON LEFT CREASE BEAM BETWEEN BS 307 AND 310. REMOVED AND REPLACED SECTION BETWEEN BS 307 AND BS 310. ALODINE, PRIMED, AND INSTALLED RE - [SDR TSAA0357117](https://openairdocs.org/sdr/TSAA0357117), May 7, 2003: WEB. CORRODED. CORROSION DISCOVERED ON RIGHT WING SPAR WEB AT FSS 540-552 BEHIND THE NR 6 SLAT. CUTOUT DAMAGED SECTION OF WEB. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOL - [SDR TSAA0353133](https://openairdocs.org/sdr/TSAA0353133), May 6, 2003: FLOORBEAM. CORRODED. FOUND CORROSION DISCOVERED AT BS 312 FLOORBEAM UPPER TEE. CUTOUT DAMAGED SECTION OF STRINGER. FABRIATED NEW CHORD SECTION AND SPLICE ANGLE. DRILLED FASTENER HOL - [SDR TSAA0353132](https://openairdocs.org/sdr/TSAA0353132), May 6, 2003: STRINGER. CRACKED. CRACK DISCOVERED ON STRINGER 4 LEFT, LOCATED AT BS 907. CUTOUT DAMGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DIRLLED FASTENER HOLES. ALODINE, PRIMED, - [SDR TSAA0353120](https://openairdocs.org/sdr/TSAA0353120), May 6, 2003: SKIN. DENTED. DENT DISCOVERED ON FUSELAGE SKIN BETWEEN BS 981 AND 996 ALONG STRINGER 14L. CUTOUT DAMAGED SECTION OF SKIN AND STRINGER. FABRICATED A REPAIR DOUBLER AND TRIPLER - [SDR TSAA0353119](https://openairdocs.org/sdr/TSAA0353119), May 6, 2003: STRINGER. DENTED. DENT DISCOVERED AT BS 376 ALONG STRINGER 17L. CUTOUT DAMAGED SECTION OF SKIN AND STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENERS HOLES. ALODINE, PRIMED, - [SDR TSAA0353118](https://openairdocs.org/sdr/TSAA0353118), May 6, 2003: STRINGER. CORRODED. CORROSION DISCOVERED ON STRINGER LOCATED AT BS 967, LBL 7. CUTOUT DAMAGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIM - [SDR TSAA0353138](https://openairdocs.org/sdr/TSAA0353138), May 5, 2003: SKIN. DENTED. DISCOVERED A 15 INCH GOUGE WITH A DENT LOCATED AT BS 981 THROUGH BS 996, 4 INCHES ABOVE STRINGER 4 LT. CUTOUT GOUGE AND DENTED PORTION OF THE SKIN. FABRICATED D - [SDR TSAA0353139](https://openairdocs.org/sdr/TSAA0353139), May 5, 2003: SKIN. DENTED. DISCOVERED A DENT LOCATED AT BS 346, BETWEEN STRINGER 24 AND 25 RIGHT. CUTOUT DENTED PORTION OF THE SKIN. FABRICATED A REPAIR PLATE, DRILLED FASTENER HOLES, ALO - [SDR TSAA0353137](https://openairdocs.org/sdr/TSAA0353137), May 5, 2003: SKIN. DENTED. DENT DISCOVERED AT BS 376 ALONG STRINGER 17 LT. CUTOUT DENTED PORTION OF THE SKIN. FABRICATED REPAIR PLATE, DRILLED FASTENER HOLES, ALODINED, PRIMED AND INSTALL - [SDR TSAA0353141](https://openairdocs.org/sdr/TSAA0353141), May 5, 2003: STRINGER CLIP. DAMAGED. DISCOVERED A DAMAGED STRINGER CLIP LOCATED AT BS 380, STRINGER 2 RIGHT. REMOVED AND REPLACED DAMAGED CLIP. ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH - [SDR TSAA0353140](https://openairdocs.org/sdr/TSAA0353140), May 5, 2003: SHEAR TIE. DAMAGED. DISCOVERED A DAMAGED SHEAR TIE LOCATED AT BS 360, BETWEEN STRINGER 14 AND 15 RIGHT. CUTOUT DENTED PORTION. FABRICATED A NEW SHEAR TIE, DRILLED FASTENER HOLES, A - [SDR TSAA0351142](https://openairdocs.org/sdr/TSAA0351142), May 5, 2003: ANGLE. CRACKED. DISCOVERED A CRACKED ATTACHMENT ANGLE LOCATED AT BS 289, WL 239. REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET W - [SDR TSAA0353136](https://openairdocs.org/sdr/TSAA0353136), May 5, 2003: STRINGER. CORRODED. CORROSION DISCOVERED AT BS 967, LBL 7, AND WL 171. CUTOUT DAMAGED PORTION OF THE STRINGER. FABRICATED NEW STRINGER SECTION, DRILLED FASTENER HOLES, ALODINED, PR - [SDR TSAA0353135](https://openairdocs.org/sdr/TSAA0353135), May 5, 2003: WEB. CORRODED. CORROSION DISCOVERED BETWEEN FSS 540 AND 552 BEHIND THE NR 6 SLAT. CUTOUT DAMAGED PORTION OF THE WEB. FABRICATED NEW WEB SECTION, DRILLED FASTENER HOLES, ALODIN - [SDR TSAA0353134](https://openairdocs.org/sdr/TSAA0353134), May 5, 2003: SHEAR TIE. DAMAGED. DAMAGED SHEAR TIE DISCOVERED AT BD 908 BETWEEN STRINGERS 14 AND 15 LEFT. CUTOUT DAMAGED SECTION. FABRICATED NEW SHEAR TIE, DRILLED FASTENER HOLES, ALODINED, PRI - [SDR TSAA0351124](https://openairdocs.org/sdr/TSAA0351124), May 5, 2003: STRINGER CLIP. CRACKED. CLIP DISCOVERED CRACKED OR TORN ON STRINGER 2R LOCATED AT BS 380. REMOVED DAMAGED CLIP. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIMED, AND - [SDR TSAA0353121](https://openairdocs.org/sdr/TSAA0353121), May 5, 2003: SHEAR TIE. DAMAGED. DAMAGE DISCOVERED ON SHEER TIE BETWEEN STRINGER 14 AND 15L AT BS 360. CUTOUT DAMAGED SECTION OF SHEAR TIE. FABRICATED A REPAIR SHEAR TIE AND RADIUS FILLER. ALOD - [SDR TSAA0353123](https://openairdocs.org/sdr/TSAA0353123), May 5, 2003: SKIN. DENTED. DENT LOCATED AT BS 396 BETWEEN STRINGER 24 AND 25R. CUTOUT DAMAGED SECTION OF STRINGER. FABRICATED A NEW STRINGER REPAIR SECTION. ALODINE, PRIMED, AND INSTALLED - [SDR TSAA0351143](https://openairdocs.org/sdr/TSAA0351143), May 5, 2003: STRINGER. DAMAGED. DAMAGED STRINGER 2 RIGHT WHILE REMOVING STRINGER CLIP. CUTOUT DAMAGED STRINGER SECTION BETWEEN BS 360 AND BS 389. FABRICATED NEW STRINGER SECTION, ALODINED, PRI - [SDR TSAA0351148](https://openairdocs.org/sdr/TSAA0351148), May 4, 2003: CHANNEL. CORRODED. FOUND CORROSION ON C-CHANNEL UPPER STRUCTURE LOCATED BETWEEN BS 312 AND BS 344 AT WL 208, LBL 57. REMOVED AND REPLACED ENTIRE SECTION BETWEEN BS 312 AND BS 344. - [SDR TSAA0353149](https://openairdocs.org/sdr/TSAA0353149), May 4, 2003: CREASE BEAM. CORRODED. FOUND CORROSION ON RIGHT CREASE BEAM AROUND NUT PLATE HOLES BETWEEN BS 290 AND 358. REMOVED AND REPLACED ENTIRE SECTION BETWEEN BS 290 AND BS 358. ALODINE, PRIM - [SDR TSAA0353151](https://openairdocs.org/sdr/TSAA0353151), Apr 30, 2003: STRINGER. GOUGED. DAMAGED OR GOUGE STRINGER DISCOVERED AT BS 382. CUTOUT GOUGED AREA. FABRICATED FILLER, ALODINED, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A F - [SDR TSAA0353110](https://openairdocs.org/sdr/TSAA0353110), Apr 23, 2003: FRAME. CRACKED. FOUND BS 244 FRAME CRACKED AT RIGHT CREASE BEAM. CUT OUT DAMAGED SECTION. FABRICATED REPAIR PARTS AND DRILLED FASTENERS HOLES. ALODINE, PRIMED, AND INSTALLED RE - [SDR TSAA0353111](https://openairdocs.org/sdr/TSAA0353111), Apr 23, 2003: FLOORBEAM. CORRODED. FOUND CORROSION ON UPPER FLOORBEAM AT BS 344 BLENDED OUT 1 INCH BY 1 INCH AREA IN TWO PLACES. CUTOUT DAMAGED AREA. FABRICATED NEW FLOORBEAM SECTION PER TABLE II - [SDR TSAA0333021](https://openairdocs.org/sdr/TSAA0333021), Feb 2, 2003: BATTERY PACK. INCORRECT. REPLACED FORWARD ENTRY EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR TSAA0233215](https://openairdocs.org/sdr/TSAA0233215), Oct 15, 2002: BATTERY PACK. DISCHARGED. REPLACED NR 1,2,4, AND 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK, OK. AIRCRAFT RETURNED TO SERVICE. - [SDR TSAA0253203](https://openairdocs.org/sdr/TSAA0253203), Oct 1, 2002: SKIN. GOUGED. REMOVED DAMAGE ON FWD CARGO DOOR CUT OUT. PERFORMED A DETAILED VISUAL AND HFEC INSPECTION OF THE CUTOUT AND ALL LAP SPLICE FASTENERS HOLES IN THE REPAIR AREA, N - [SDR TSAA0225160](https://openairdocs.org/sdr/TSAA0225160), Jul 11, 2002: SLIDE. DEFECTIVE. DURING A ROUTINE TRAINING EXERCISE AND AFTER SUCCESSFUL SLIDE DEPLOYMENT, THE SLIDE ASSEMBLY EXPLODED AT THE SEAM. NO HARM TO PERSONNEL. REMOVED AND REPLACED SL - [SDR P2EA2002M040](https://openairdocs.org/sdr/P2EA2002M040), Jun 12, 2002: ACOUSTIC PANEL. GOUGED. ON WALKAROUND, FOUND THE NR 2 ENGINE TAIL PIPE EXTENSION WITH GOUGE IN ACOUSTIC PANEL 4 INCHES LONG, .0625 INCH WIDE AND .5 INCH DEEP. WELD GOUGE ACCORDING TO M - [SDR TSAA0232137](https://openairdocs.org/sdr/TSAA0232137), May 12, 2002: SWITCH. STUCK. ANTI-SKID INOPERATIVE LIGHT ILLUMINATED ON BOTH SYSTEMS DURING FLIGHT. DUE TO WEATHER CONDITIONS, RUNWAY LENGTH AND AIRCRAFT WEIGHT FOR THE AIRPORT, THE AIRCRAF - [SDR P2EA2002V0032](https://openairdocs.org/sdr/P2EA2002V0032), Apr 6, 2002: LINK. LOOSE. DURING EVALUATION FLIGHT AFTER Q1 AND Q2 INSPECTION, NR 1 ENGINE OIL QUANTITY STARTED DECREASING AFTER TAKEOFF, ENGINE NR 1 SHUTDOWN UPON TOUCHDOWN WITH 0.750 G - [SDR P2EA2002V0020](https://openairdocs.org/sdr/P2EA2002V0020), Mar 9, 2002: SKIN. -During Q1+Q2 inspection.-IMPROPER REPAIR LOCATED AT BS 1000 STR 14L.-Existing repair replaced IAW E.O. No.B737HC53-022/02, Dated March 15, 2002, approved with - [SDR P2EA2002V0026](https://openairdocs.org/sdr/P2EA2002V0026), Mar 3, 2002: -DURING Q1 AND Q2 INSPECTION:-RUDDER STA 85 SKIN WITH DENT-REPAIRED IAW EO B737HC57-051/02. APPROVED 8110-3 DTD 03-06-02 BY FAA DER ROBERT MANASHI (DERT-71067-S - [SDR P2EA2002V0021](https://openairdocs.org/sdr/P2EA2002V0021), Feb 21, 2002: SKIN. -During Q1+Q2 inspection.-IMPROPER REPAIR LOCATED AT BS 259 STR 19L.-Existing repair replaced IAW E.O. No.B737HC53-023/02, Dated March 15, 2002, approved with F - [SDR P2EA2002V0029](https://openairdocs.org/sdr/P2EA2002V0029), Feb 20, 2002: BEAM. CORRODED. DURING Q1 AND Q2 INSPECTION, RT HORIZONTAL STABILIZER LWR AREA T/E BEAM WITH CORROSION BETWEEN ELEV STA 94.07 AND ELEV STA 100. RT HORIZONTAL STABILIZER LWR ARE - [SDR P2EA2002V0028](https://openairdocs.org/sdr/P2EA2002V0028), Feb 20, 2002: STRINGER. CORRODED. DURING Q1 AND Q2 INSPECTION, BETWEEN BS 967 AND BS 986.5 STR 23L WITH CORROSION. STRINGER REPAIRED IAW SRM 53-10-3 FIG 1. - [SDR P2EA2002V0027](https://openairdocs.org/sdr/P2EA2002V0027), Feb 20, 2002: SPAR. DELAMINATED. DURING Q1 AND Q2 INSPECTION, LT WING AILERON FRONT SPAR LOWER CHORD WITH DELAMINATION SPOTS BETWEEN WBL 417.250 AND WBL 251.8. REPAIRED IAW EO B737HC57-008/02 A - [SDR P2EA2002V0025](https://openairdocs.org/sdr/P2EA2002V0025), Feb 20, 2002: AILERON. DELAMINATED. RIGHT WING AILERON DELAMINATED BETWEEN WBL 417 AND WBL 446. REPAIRED IAW EO B737HC57-007/02 APPROVED 8110-3 FORM BY FAA. All 161: https://openairdocs.org/model/boeing-737-25a/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.