# Service difficulty reports: Boeing 737-25A

A list on [Boeing 737-25A](https://openairdocs.org/model/boeing-737-25a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 161 reports

- [SDR TSAA0524018](https://openairdocs.org/sdr/TSAA0524018.md): Circuit Breaker · damaged · Apr 4, 2005 · N819AL · Boeing 73725A · DC Power Distribution System
  > 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 NOT CURE PROBLEM. FOUND B-LEG ON APU GENERATOR DEAD. DEFER PER MEL 24-2. PLACARDS INSTALLED
- [SDR TSAA0421081](https://openairdocs.org/sdr/TSAA0421081.md): Clamp · loose · Nov 30, 2004 · N819AL · Boeing 73725A · Air Distribution System
  > 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 DEACTIVATED PRIOR TO THIS FLIGHT DUE TO REPORTS OF A WHOOSHING SOUND NEAR ROW 7 & 8. THE FIRST OFFICER F
- [SDR TSAA0472079](https://openairdocs.org/sdr/TSAA0472079.md): Engine · failed · Nov 27, 2004 · N819AL · Boeing 73725A · Engine (Turbine/Turboprop)
  > 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. REPORTED THAT A PASSENGER OBSERVED FLAMES EXITING THE NR 2 ENGINE EXHAUST. ALL OTHER ENGINE INDICATIONS
- [SDR TSAA0473068](https://openairdocs.org/sdr/TSAA0473068.md): Fcu · malfunctioned · Sep 14, 2004 · N819AL · Boeing 73725A · Fuel Control/Turbine Engines
  > 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 94 PERCENT; FURTHER THRUST LEVER MOVEMENT HAD NO EFFECT. REMOVED AND REPLACED THE NR 1 ENGINE FCU
- [SDR TSAA0431067](https://openairdocs.org/sdr/TSAA0431067.md): Indicator · slow · Sep 12, 2004 · N819AL · Boeing 73725A · Airspeed/Mach Indicator
  > 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 INDICATOR. RETURNED TO HNL. CLEARED FIRST-OFFICERS PITOT TUBE OF DEBRIS IAW AMM 34-11-0, LEAK AND
- [SDR TSAA0477066](https://openairdocs.org/sdr/TSAA0477066.md): Engine · malfunctioned · Sep 11, 2004 · N819AL · Boeing 73725A · Engine (Turbine/Turboprop)
  > 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 LINES. PERFORMED ENGINE RUN FOR TAKEOFF POWER VERIFICATION, OPS CHECK OK. AIRCRAFT RETURNED TO S
- [SDR RYN2004F00019](https://openairdocs.org/sdr/RYN2004F00019.md): Doubler · torn · May 3, 2004 · N8878Z · Boeing 73725A · Fuselage Miscellaneous Structure
  > AT C-CHECK, FOUND TEAR IN R-1 DOOR THRESHOLD DOUBLER, AT STATION 392.
- [SDR TSAA0452026](https://openairdocs.org/sdr/TSAA0452026.md): Door Frame · corroded · Feb 4, 2004 · N819AL · Boeing 73725A · Fuselage Main, Structure
  > FOUND CORROSION ON FORWARD CARGO DOOR FRAME. TRIMMED OUT DAMAGED AREA. HFEC VERIFIED CRACK REMOVED. FABRICATED REPAIR DOUBLERS AND TRIPLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAIR PARTS MAKING A FAYING SEAL AROUND REPAIR. REPAIR COMPLETED
- [SDR TSAA0477018](https://openairdocs.org/sdr/TSAA0477018.md): Circuit Breaker · tripped · Jan 9, 2004 · N819AL · Boeing 73725A · Engine Pressure Ratio (EPR)
  > 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. AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR TSAA0333147](https://openairdocs.org/sdr/TSAA0333147.md): Battery Pack · inoperative · Jun 7, 2003 · N819AL · Boeing 73725A · Emergency Lighting
  > 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.md): Battery Pack · inoperative · Jun 7, 2003 · N819AL · Boeing 73725A · Emergency Lighting
  > 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.md): Crease Beam · corroded · May 22, 2003 · N819AL · Boeing 73725A · Fuselage Main, Structure
  > 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 REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-30-2 AND
- [SDR TSAA0357117](https://openairdocs.org/sdr/TSAA0357117.md): Web · corroded · May 7, 2003 · N819AL · Boeing 73725A · Leading Edge Devices
  > 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 HOLES. ALODINE, PRIMED AND INSTALLED REPAIR PART WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. RE
- [SDR TSAA0353133](https://openairdocs.org/sdr/TSAA0353133.md): Floorbeam · corroded · May 6, 2003 · N819AL · Boeing 73725A · Fuselage Main, Floor Beam
  > FOUND CORROSION DISCOVERED AT BS 312 FLOORBEAM UPPER TEE. CUTOUT DAMAGED SECTION OF STRINGER. FABRIATED NEW CHORD SECTION AND SPLICE ANGLE. DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL.
- [SDR TSAA0353132](https://openairdocs.org/sdr/TSAA0353132.md): Stringer · cracked · May 6, 2003 · N819AL · Boeing 73725A · Fuselage Main, Longeron/Stringer
  > CRACK DISCOVERED ON STRINGER 4 LEFT, LOCATED AT BS 907. CUTOUT DAMGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DIRLLED FASTENER HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW
- [SDR TSAA0353120](https://openairdocs.org/sdr/TSAA0353120.md): Skin · dented · May 6, 2003 · N819AL · Boeing 73725A · Fuselage Main, Plate/Skin
  > 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. ALODINE, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. RE
- [SDR TSAA0353119](https://openairdocs.org/sdr/TSAA0353119.md): Stringer · dented · May 6, 2003 · N819AL · Boeing 73725A · Fuselage Main, Longeron/Stringer
  > DENT DISCOVERED AT BS 376 ALONG STRINGER 17L. CUTOUT DAMAGED SECTION OF SKIN AND STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENERS HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IA
- [SDR TSAA0353118](https://openairdocs.org/sdr/TSAA0353118.md): Stringer · corroded · May 6, 2003 · N819AL · Boeing 73725A · Fuselage Main, Longeron/Stringer
  > CORROSION DISCOVERED ON STRINGER LOCATED AT BS 967, LBL 7. CUTOUT DAMAGED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND DRILLED FASTENER HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED
- [SDR TSAA0353138](https://openairdocs.org/sdr/TSAA0353138.md): Skin · dented · May 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Plate/Skin
  > 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 DOUBLER AND TRIPLER, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH
- [SDR TSAA0353139](https://openairdocs.org/sdr/TSAA0353139.md): Skin · dented · May 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Plate/Skin
  > 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, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR
- [SDR TSAA0353137](https://openairdocs.org/sdr/TSAA0353137.md): Skin · dented · May 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Plate/Skin
  > DENT DISCOVERED AT BS 376 ALONG STRINGER 17 LT. CUTOUT DENTED PORTION OF THE SKIN. FABRICATED REPAIR PLATE, DRILLED FASTENER HOLES, ALODINED, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-3
- [SDR TSAA0353141](https://openairdocs.org/sdr/TSAA0353141.md): Stringer Clip · damaged · May 5, 2003 · N819AL · Boeing 73725A · Fuselage Miscellaneous Structure
  > 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 FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-30-2, FIGURE 1. (M)
- [SDR TSAA0353140](https://openairdocs.org/sdr/TSAA0353140.md): Shear Tie · damaged · May 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Structure
  > 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, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPA
- [SDR TSAA0351142](https://openairdocs.org/sdr/TSAA0351142.md): Angle · cracked · May 5, 2003 · N819AL · Boeing 73725A · Fuselage Miscellaneous Structure
  > DISCOVERED A CRACKED ATTACHMENT ANGLE LOCATED AT BS 289, WL 239. REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-30-2. (M)
- [SDR TSAA0353136](https://openairdocs.org/sdr/TSAA0353136.md): Stringer · corroded · May 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Longeron/Stringer
  > CORROSION DISCOVERED AT BS 967, LBL 7, AND WL 171. CUTOUT DAMAGED PORTION OF THE STRINGER. FABRICATED NEW STRINGER SECTION, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETE
- [SDR TSAA0353135](https://openairdocs.org/sdr/TSAA0353135.md): Web · corroded · May 5, 2003 · N819AL · Boeing 73725A · Fuselage Miscellaneous Structure
  > 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, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR CO
- [SDR TSAA0353134](https://openairdocs.org/sdr/TSAA0353134.md): Shear Tie · damaged · May 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Structure
  > DAMAGED SHEAR TIE DISCOVERED AT BD 908 BETWEEN STRINGERS 14 AND 15 LEFT. CUTOUT DAMAGED SECTION. FABRICATED NEW SHEAR TIE, DRILLED FASTENER HOLES, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED
- [SDR TSAA0351124](https://openairdocs.org/sdr/TSAA0351124.md): Stringer Clip · cracked · May 5, 2003 · N819AL · Boeing 73725A · Fuselage Miscellaneous Structure
  > 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 INSTALLED REPAIR PARTS. REPAIR COMPLETED IAW SRM 51-30-2, FIGURE 1. (M)
- [SDR TSAA0353121](https://openairdocs.org/sdr/TSAA0353121.md): Shear Tie · damaged · May 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Structure
  > 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. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR
- [SDR TSAA0353123](https://openairdocs.org/sdr/TSAA0353123.md): Skin · dented · May 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Plate/Skin
  > 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 REPAR PART IAW FASTENERS FROM TABLE 1 MAKING A FAYING SEAL. REPAIR COMPLETED IAW SRM 53-30-3, F
- [SDR TSAA0351143](https://openairdocs.org/sdr/TSAA0351143.md): Stringer · damaged · May 5, 2003 · N819AL · Boeing 73725A · Fuselage Main, Longeron/Stringer
  > DAMAGED STRINGER 2 RIGHT WHILE REMOVING STRINGER CLIP. CUTOUT DAMAGED STRINGER SECTION BETWEEN BS 360 AND BS 389. FABRICATED NEW STRINGER SECTION, ALODINED, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED
- [SDR TSAA0351148](https://openairdocs.org/sdr/TSAA0351148.md): Channel · corroded · May 4, 2003 · N819AL · Boeing 73725A · Fuselage Miscellaneous Structure
  > 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. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REP
- [SDR TSAA0353149](https://openairdocs.org/sdr/TSAA0353149.md): Crease Beam · corroded · May 4, 2003 · N819AL · Boeing 73725A · Fuselage Main, Structure
  > 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, PRIMED, AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED
- [SDR TSAA0353151](https://openairdocs.org/sdr/TSAA0353151.md): Stringer · gouged · Apr 30, 2003 · N819AL · Boeing 73725A · Fuselage Main, Longeron/Stringer
  > DAMAGED OR GOUGE STRINGER DISCOVERED AT BS 382. CUTOUT GOUGED AREA. FABRICATED FILLER, ALODINED, PRIMED AND INSTALLED REPAIR PARTS WET WITH FASTENERS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 53-10-3, FIGURE 3. (M)
- [SDR TSAA0353110](https://openairdocs.org/sdr/TSAA0353110.md): Frame · cracked · Apr 23, 2003 · N819AL · Boeing 73725A · Fuselage Main, Frame
  > FOUND BS 244 FRAME CRACKED AT RIGHT CREASE BEAM. CUT OUT DAMAGED SECTION. FABRICATED REPAIR PARTS AND DRILLED FASTENERS HOLES. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS MAKING A FAYING SURFACE SEAL. REPAIR COMPLETED IAW SRM 51-40-3, FIGURE 1. (M)
- [SDR TSAA0353111](https://openairdocs.org/sdr/TSAA0353111.md): Floorbeam · corroded · Apr 23, 2003 · N819AL · Boeing 73725A · Fuselage Main, Floor Beam
  > 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, DETAIL I. ALODINE, PRIMED, AND INSTALLED REPAIR PARTS WET MAKING A FAYING SURFACE SEAL. REPAIR CO
- [SDR TSAA0333021](https://openairdocs.org/sdr/TSAA0333021.md): Battery Pack · incorrect · Feb 2, 2003 · N819AL · Boeing 73725A · Emergency Lighting
  > 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.md): Battery Pack · discharged · Oct 15, 2002 · N819AL · Boeing 73725A · Emergency Lighting
  > 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.md): Skin · gouged · Oct 1, 2002 · N819AL · Boeing 73725A · Fuselage Main, Plate/Skin
  > 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, NO DEFECTS NOTED. INSTALLED REPAIR IAW SRM. AIRCRAFT RETURNED TO SERVICE.(TSAA8003321)
- [SDR TSAA0225160](https://openairdocs.org/sdr/TSAA0225160.md): Slide · defective · Jul 11, 2002 · N819AL · Boeing 73725A · Escape Slide
  > DURING A ROUTINE TRAINING EXERCISE AND AFTER SUCCESSFUL SLIDE DEPLOYMENT, THE SLIDE ASSEMBLY EXPLODED AT THE SEAM. NO HARM TO PERSONNEL. REMOVED AND REPLACED SLIDE; CONTINUED WITH EXERCISE. SLIDE SENT TO VENDOR FOR EVALUATION.
- [SDR P2EA2002M040](https://openairdocs.org/sdr/P2EA2002M040.md): Acoustic Panel · gouged · Jun 12, 2002 · N239TA · Boeing 73725A · Engine Collector/Tailpipe/Nozzle
  > 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 MM 78-38-43.
- [SDR TSAA0232137](https://openairdocs.org/sdr/TSAA0232137.md): Switch · stuck · May 12, 2002 · N819AL · Boeing 73725A · Landing Gear Selector
  > ANTI-SKID INOPERATIVE LIGHT ILLUMINATED ON BOTH SYSTEMS DURING FLIGHT. DUE TO WEATHER CONDITIONS, RUNWAY LENGTH AND AIRCRAFT WEIGHT FOR THE AIRPORT, THE AIRCRAFT RETURNED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED A DEFECTIVE LANDING GEAR LEVER UP SWITCH
- [SDR P2EA2002V0032](https://openairdocs.org/sdr/P2EA2002V0032.md): Link · loose · Apr 6, 2002 · N239TA · Boeing 73725A · Engine Oil Storage (Airframe Furnished)
  > 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 GALS. PRESSURE LINK TIGHTENED AT OIL FILTER BYPASS SW IAW MM 20-50-11 PAGE 211, ENGINE OIL SERVICED
- [SDR P2EA2002V0020](https://openairdocs.org/sdr/P2EA2002V0020.md): Skin · Mar 9, 2002 · N239TA · Boeing 73725A · Fuselage Main, Plate/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 FAA 8110-3 form submited by P.C.LeBar.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0715, SDA No. 2
- [SDR P2EA2002V0026](https://openairdocs.org/sdr/P2EA2002V0026.md): Service difficulty · Mar 3, 2002 · N239TA · Boeing 73725A · Vertical Stabilizer, Plate/Skin
  > -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-SW)-NOTE: SEE AEROMAN W/O No. 2002-90/1, VAM100 0579, SDA 239SDA030
- [SDR P2EA2002V0021](https://openairdocs.org/sdr/P2EA2002V0021.md): Skin · Feb 21, 2002 · N239TA · Boeing 73725A · Fuselage Main, Plate/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 FAA 8110-3 form submited by B.R.Frakes.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0714, SDA No. 2
- [SDR P2EA2002V0029](https://openairdocs.org/sdr/P2EA2002V0029.md): Beam · corroded · Feb 20, 2002 · N239TA · Boeing 73725A · Horizontal Stabilizer Miscellaneous Structure
  > 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 AREA T/E BEAM REPAIRED IAW SRM 55-107 FIG 1.
- [SDR P2EA2002V0028](https://openairdocs.org/sdr/P2EA2002V0028.md): Stringer · corroded · Feb 20, 2002 · N239TA · Boeing 73725A · Fuselage Main, Longeron/Stringer
  > 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.md): Spar · delaminated · Feb 20, 2002 · N239TA · Boeing 73725A · Ailerons
  > 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 APPROVED BY 8110-3 FORM BY FAA.
- [SDR P2EA2002V0025](https://openairdocs.org/sdr/P2EA2002V0025.md): Aileron · delaminated · Feb 20, 2002 · N239TA · Boeing 73725A · Ailerons
  > RIGHT WING AILERON DELAMINATED BETWEEN WBL 417 AND WBL 446. REPAIRED IAW EO B737HC57-007/02 APPROVED 8110-3 FORM BY FAA.

Next page: https://openairdocs.org/model/boeing-737-25a/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '73725A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-737-25a/reports

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