Boeing 737-25A

Service difficulty reports · 161

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR P2EA2002V0024Service difficulty-During Q1+Q2 inspection.-L-H WING IMB. FORE FLAP WITH UPPER SKIN DELAMINATED.-Repaired IAW E.O. No. B737HC57-006/02, DATED Feb 27, 2002 approved with FAA 8110-3 form, submited by Robert Manashi, (DERT-710167-SW).Note: See Aeroman W/O No. 2002-90/1, VAM100 No.Feb 20, 2002 · N239TA · Boeing 73725A · Trailing Edge FlapsSDR P2EA2002V0023Service difficulty-During Q1+Q2 inspection.-RH WING AILERON TAB BROKEN NEAR INBD AND OUTBD CENTER HINGE ASSEMBLY.-Repaired cracks IAW E.O. No. B737HC57-012/02, DATED March 08, 2002 approved with FAA 8110-3 form, submited by Robert Manashi, (DERT-710167-SW).Note: See Aeroman W/OFeb 20, 2002 · N239TA · Boeing 73725A · Aileron TabsSDR P2EA2002V0022Fitting-During Q1+Q2 inspection.-VERTICAL STABILIZER SUPPORT FITTING WITH CRACK AT REAR SPAR CAVITY FIN STA 90.3.-Rudder support fitting repaired IAW E.O. No. B737HC55-007/02, DATED Feb 15, 2002 approved with FAA 8110-3 form, submited by Robert Manashi, (DERT-710167-Feb 20, 2002 · N239TA · Boeing 73725A · Ventral StructureSDR P2EA2002V0014Frame-During Q1+Q2 inspection.-FWD CARGO COMPARTMENT AT BS 492.4 ATR 24R FRAME WITH CRACK.-Frame repaired IAW SRM 51-40-3, Fig 1.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.314, SDA No. 239SDA017.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, FrameSDR P2EA2002V0013Frame · bentDURING Q1+ Q2 INSPECTION, FWD CARGO COMPARTMENT BS 420 STR 24L FRAME BENT. FRAME REPAIRED IAW SRM 51-40-3 FIG 1.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, FrameSDR P2EA2002V0030Seat Track-DURING Q1 AND Q2 INSPECTION:-PAX CABIN BS 380 AND RBL 45.5 SEAT TRACK WITH CORROSION -SEAT TRACK REPAIRED IAW SRM 53-10-5 FIG. 2-NOTE: SEE AEROMAN W/O No. 2002-90/1, VAM100 0583, SDA 239SDA097Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, StructureSDR P2EA2002V018Angle · crackedDURING Q1+Q2 INSPECTION, MAIN PASSENGER CABIN FLOOR AREA AT STA 520 FLOOR ANGLE CRACKED. FLOOR ANGLE REPAIRED IAW SRM 51-40-4 FIG 1 DETAIL 5.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Miscellaneous StructureSDR P2EA2002V0009Floorbeam · corrodedDURING Q1+Q2 INSPECTION, PAX CABIN RBL 12 BS 360 FLOORBEAM WITH CORROSION. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 1.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2000V0008Floorbeam · corrodedDURING Q1+Q2 INSPECTION, AFT GALLEY AREA BS 1016 LBL 33 FLOORBEAM WITH CORROSION. FLOORBEAM REPAIRED IAW EO B737MC53-019/02, BOEING SL 737-SL-53-036 AND DWG NR 65C37528, 65C37472.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0007Floorbeam · corrodedDURING Q1+Q2 INSPECTION, PAX CABIN BS 294.5 FLOORBEAM UPPER CHORD LWR SURFACE WITH CORROSION RBL 24. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 6.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2000V0003Floorbeam · corrodedDURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 344 BTW LBL 14 AND LBL 21. FLOORBEAM REPAIRED IAW SRM 53-10-9, FIG 5.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0002Floorbeam · corrodedDURING Q1+Q2 INSPECTION, PAX CABIN FLOORBEAM UPPER CHORD WITH CORROSION AT BS 947.5 BETWEEN LBL 5 AND RBL 5. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 2.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0001Floorbeam · scratchedDURING Q1+Q2 INSPECTION, PAX CABIN AT BS 380 BETWEEN RBL 24.5 AND RBL 45.5 FLOORBEAM UPPER CHORD WITH SCRATCH. SCRATCH REPAIRED IAW SRM 53-10-9 FIG 1.Feb 19, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0016Stringer-During Q1+Q2 inspection.-INTERNAL FUSELAGE STR 16L WITH CRACK BTW BS 520 AND SCANNING LIGHT BASE.-Scaqnning ligth base at Str 16L-H repaired IAW E.O. No. B737MC53-18/02 & S/B 737-53-1145.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0322, SDA No. 239SDA019.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, Longeron/StringerSDR P2EA2002V0015Stringer-During Q1+Q2 inspection.-INTERNAL FUSELAGE STR 16R WITH CRACK BTW BS 520 AND SCANNING LIGHT BASE.-Scaqnning ligth base at Str 16R-H repaired IAW E.O. No. B737MC53-18/02 & S/B 737-53-1145.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0321, SDA No. 239SDA018.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, FrameSDR P2EA2002V0012Frame-During Q1+Q2 inspection.-BS 420 AT STR 26LH FRAME WITH CRACK.-Frame upper flange repaired IAW SRM 51-40-3, Fig1.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.076, SDA No. 239SDA005.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, FrameSDR P2EA2002V0011Frame-During Q1+Q2 inspection.-BS 460 AT STR 26LH FRAME WITH CRACK.-Frame repaired IAW SRM 51-40-3, Fig 1.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.073, SDA No. 239SDA004.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, FrameSDR 2PEA2002V0017Service difficulty-During Q1+Q2 inspection.-RIGHT WING FORE FLAP EXISTING REPAIR FROM WBL227 TO 254 FOUND WITH GOUGE.-Doubler of existing repair replaced IAW SRM 51-10-1, Fig 1, between WBL250 to WBL254, repair accomplished IAW SRM 57-50-4, Fig 1.Note: See Aeroman W/O No. 2002-Feb 18, 2002 · N239TA · Boeing 73725A · Trailing Edge FlapsSDR P2EA2002V0006Floorbeam · corrodedDURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 294.5 BL 0. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 5.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0005Floorbeam · corrodedDURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 312 AND LBL 8. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 5.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0004Floorbeam · corrodedDURING Q1+Q2 INSPECTION, PASSENGER CABIN FLOORBEAM WITH CORROSION AT BS 328 AND LBL 28. FLOORBEAM REPAIRED IAW SRM 53-10-9 FIG 6.Feb 18, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0010Floorbeam · crackedDURING Q1+Q2 INSPECTION, LONGITUDINAL FLOORBEAM AT BL 0, BS 663 UPPER CHORD CRACKED. LONGITUDINAL FLOORBEAM REPAIRED IAW EO B737MC57-010/02, S/B 737-57-1210.Feb 17, 2002 · N239TA · Boeing 73725A · Fuselage Main, Floor BeamSDR P2EA2002V0019Service difficulty-During Q1+Q2 inspection.-RH WING FORE FLAP AT WSL 479 LOWER SURFACE WITH SEVERAL GOUGES.-R-H wing Fore flap repaired IAW SRM 57-40-4, Fig 1.Note: See Aeroman W/O No. 2002-90/1, VAM100 No.0160, SDA No. 239SDA009.Feb 15, 2002 · N239TA · Boeing 73725A · Trailing Edge FlapsSDR P2EA2002V0031SkinDURING Q1 AND Q2 INSPECTION:-E/E COMPARTMENT DOOR WITH NICK ON SKIN EDGES STA 325.18-NICK REPAIRED IAW SRM 737-200 52-00-3 FIG.5-NOTE: SEE AEROMAN W/O No. 2002-90/1, VAM100 0012, SDA 239SDA112Feb 14, 2002 · N239TA · Boeing 73725A · Electrical/Electronic Compartment DoorsSDR P2EA2002M006Clamp · looseAPU FIRE LIGHT CAME ON IN FLIGHT. FIRE HANDLE PULLED AND FIRE BOTTLE DISCHARGED. LIGHT WENT OUT AFTER 10 MINUTES. FOUND AN APU BLEED AIR DUCT WITH LOOSE CLAMP THAT WAS BLOWING ON THE FIRE DETECTION LOOP. TIGHTENED CLAMP, OPS CHECKS NORMAL.Feb 10, 2002 · N239TA · Boeing 73725A · APU Bleed Air SystemSDR P2EA2002M004Fire Detector · malfunctionedPRIOR TO PUSH BACK, APU SHUT DOWN, LATER THE APU FIRE WARNING AND BELL ILLUMINATED. PERFORMED APU FIRE CHECK LIST PROCEDURES PULLED AND ROTATED HANDLE. PERFORMED AN APU FIRE INSPECTION AND FOUND NO EVIDENCE OF FIRE. PLACED THE APU, APU FIRE DETECTION AND THFeb 3, 2002 · N239TA · Boeing 73725A · Fire DetectionSDR TSAA0257032Structure · crackedREPAIRED CRACK AT NR 5 SLAT STATION 195.53. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .050 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAGE 1 FIGURE 1. AIRJan 8, 2002 · N819AL · Boeing 73725A · Leading Edge DevicesSDR TSAA0257033Structure · crackedREPAIRED CRACK AT NR 4 SLAT STATION 35.84. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .50 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAGE 2 DETAIL II. AIRCJan 8, 2002 · N819AL · Boeing 73725A · Leading Edge DevicesSDR TSAA0253034Floorbeam · crackedFOUND CABIN INTERIOR LONGITUDINAL FLOORBEAM UPPER CHORD AND WEB CRACKED AT BS 663.75 BL 0. VERIFIED CRACK REMOVED USING HFEC. REPAIRED LONGITUDINAL FLOORBEAM IAW ECO 223R2 PART II, DEVIATION "C". AIRCRAFT RETURNED TO SERVICE. (M)Jan 8, 2002 · N819AL · Boeing 73725A · Fuselage Main, Floor BeamSDR TSAA0253035Skin · crackedREPAIRED A 4 INCH CRACK ON THE FUSELAGE SKIN AT BS 727 JUST BELOW STRINGER 18 RT. VERIFEID CUTOUT USING HFEC. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3 PAGE 11 FIGURE 6. AIRCRAFT RETURNED TO SERVICE. (M)Jan 8, 2002 · N819AL · Boeing 73725A · Fuselage Main, Plate/SkinSDR TSAA0253036Skin · crackedREPAIRED A 2.5 INCH CRACK ON THE FUSELAGE SKIN AT BS 727 JUST BELOW STRINGER 19 RT. VERIFIED CUTOUT USING HFEC. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-30-3 PAGE 11 FIGURE 6. AIRCRAFT RETURNED TO SERVICE. (M)Jan 8, 2002 · N819AL · Boeing 73725A · Fuselage Main, Plate/SkinSDR TSAA0253037Skin · delaminatedFOUND DELAMINATION ON LOWER SURFACE OF RIGHT ELEVATOR. TRIMMED OUT DAMAGED LAMINATION TO A SMOOTH SHAPE WITH ROUNDED CORNERS. FABRICATED, CLEANED AND INSTALLED HONEYCOMB REPLACEMENT CORE PLUG. PREPARED AND APPLIED REPAIR PLIES. INSTALLED HEATED BLANKET ANDJan 8, 2002 · N819AL · Boeing 73725A · Elevator, Plate/SkinSDR TSAA0257039Structure · crackedREPAIRED CRACK AT NR 4 SLAT STATION 35.84. REPAIR CONSISTS OF BLENDING OUT THE DAMAGED AREA, MAINTAINING A BLEND OUT LENGTH OF .075 INCH MAXIMUM AND USING A MINIMUM RADIUS OF .50 INCH. REMOVED ALL BURRS AND SHARP EDGES IAW SRM 57-20-1 PAGE 1 FIGURE 1. AIRCRJan 8, 2002 · N819AL · Boeing 73725A · Leading Edge DevicesSDR TSAA0253040Skin · corrodedBLENDED OUT CORROSION ON THE FUSELAGE SKIN AT BS 990 STRINGER 27L BY CUTTING STRINGER 27L IAW SRM 51-10-2. VERIFIED CORROSION REMOVED, CLEANED AND TREATED IAW SRM 51-10-6. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-20-2 FIGURE 3. AIRCRAFT RETURNED TO Jan 8, 2002 · N819AL · Boeing 73725A · Fuselage Main, Plate/SkinSDR TSAA0253041Floor Support · crackedFOUND CABIN INTERIOR LONGITUTIONAL FLOOR SUPPORT UPPER CHORD AND WEB CRACKED AT BS 663.75 BL 0. VERIFIED CRACK REMOVED USING HFEC. REPAIRED LONGITIONAL FLOORBEAM IAW ECO 2223R2 PART II, DEVIATION 'C'. AIRCRAFT RETURNED TO SERVICE. (M)Jan 8, 2002 · N819AL · Boeing 73725A · Fuselage Miscellaneous StructureSDR TSAA0257031Slat · crackedREPAIRED CRACK AT NR 6 SLAT STATION 370.56. BLENDED OUT THE DAMAGED AREA IAW SRM 57-20-1, FIG 1, PAGE 1. AIRCRAFT RETURNED TO SERVICE. (M)Jan 8, 2002 · N819AL · Boeing 73725A · Leading Edge DevicesSDR P2EA2001M0017Controller · faultyNR 2 ENGINE STALLED THREE TIMES DURING TAXI, ALSO NR 2 EPR STICKING. REMOVED AND REPLACED PRBC IAW MM 75-31-11. REMOVED AND REPLACED EPR TRANSMITTER IAW 77-11-0. OPERATIONAL CHECKS NORMAL.Dec 21, 2001 · N239TA · Boeing 73725A · Compressor Bleed ControlSDR P2EA2001M0014Csd · malfunctionedNR 1 ENGINE CSD LOW OIL PRESSURE LIGHT WOULD NOT EXTINGUISH AFTER ENGINE START. AIRCRAFT RETURNED TO BLOCKS WITH NO INCIDENT. RESET NR 1 ENGINE CSD T-HANDLE. OPERATIONAL CHECK NORMAL IAW MM 24-11-11.Dec 5, 2001 · N239TA · Boeing 73725A · Alternator-Generator DriveSDR TSAA0133172Battery Pack · dischargedREPLACED NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Dec 1, 2001 · N819AL · Boeing 73725A · Emergency LightingSDR P2EA2001M0010Start Valve · failedNR 1 ENGINE START VALVE WOULD NOT OPEN. AIRCRAFT RETURNED TO GATE. REMOVED AND REPLACED START VALVE IAW MM 80-11-21. OPERATIONAL CHECK NORMAL.Nov 10, 2001 · N239TA · Boeing 73725A · Engine Start Valves/ControlsSDR P2EA2001M0009Engine · damagedDURING TAKEOFF LOUD BANG WAS HEARD. ABORTED TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. DAMAGE REPORTED TO EXHAUST AREA OF NR 1 ENGINE. REMOVED AND REPLACED NR 1 ENGINE IAW TASK CARD J271-00-01.Oct 19, 2001 · N239NJ · Boeing 73725A · Engine (Turbine/Turboprop)SDR P2EA2001M0001Connector · dirtyAIR-CONDITION AND MASTER CAUTION ON PRE-TAKEOFF RECALL WITH NO ASSOCIATED PANEL INDICATION. RETURNED TO GATE. SUSPECTED APU BLEED VALVE. OP'S CHECKED, GOT DUAL BLEED LIGHTS WITH APU BLEED SHUT OFF, PSI HELD, DUAL BLEED LIGHTS STAYED ON. BLEED VALVE OP'S NORSep 23, 2001 · N239TA · Boeing 73725A · APU Bleed Air SystemSDR TSAA0133106Battery Pack · inoperativeREPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCAFT RETURNED TO SERVICE. (M)Aug 14, 2001 · N819AL · Boeing 73725A · Lighting SystemSDR TSAA0133031Light · inoperativeREPLACED NR 1 FLOOR PROXIMITY LIGHT ASSY FOR RETIREMENT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Mar 3, 2001 · N819AL · Boeing 73725A · Emergency LightingSDR TSAA0136007Valve · defectiveFLT 210 - HNL-OGG - DURING TAKEOFF, NR 2 ENGINE BLEED LIGHT CAME ON. ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED THE NR 2 ENGINE PNEUMATIC SHUTOFF VALVE IAW MM 21-11-011-6. OPS AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jan 21, 2001 · N819AL · Boeing 73725A · Pneumatic Distribution SystemSDR TSAA0033199Battery Pack · inoperativeREPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Aug 23, 2000 · N819AL · Boeing 73725A · Emergency LightingSDR TSAA0029077Hydraulic Line · brokenFLT 86 - HNL-KOA - DURING TAKEOFF, EXPERIENCED A COMPLETE LOSS OF A SYSTEM HYDRAULICS. PERFORMED CHECKSLIST AND RETURNED TO HNL FOR AN UNEVENTFUL LANDING. AFTER LANDIG THE STANDBY LOW QUANTITY LIGHT CAME ON. AFTER THE LANDING GEAR WAS LOWERED, WAS UNABLE TOMar 4, 2000 · N819AL · Boeing 73725A · Hydraulic System, MainSDR TSAA200033055Battery Pack · inoperativeREPLACED NR 2 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)Feb 6, 2000 · N819AL · Boeing 73725A · Emergency LightingSDR TSAA200033054Battery Pack · inoperativeREPLACED BATTERY PACK IN FORWARD SERVICE DOOR EMERGENCY EXIT IDENTIFIER LIGHT ASSY DUE TO INOPERABLE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (X)Feb 5, 2000 · N819AL · Boeing 73725A · Emergency LightingSDR TSAA9949510Apu · leakingFLT 29 - HNL-KOA - APU SHUTDOWN IN FLIGHT. INSPECTED APU AND FOUND LOW OIL QTY. APU LEAKING OIL. REMOVED AND REPLACED APU PER FORM M-133. LEAK AND OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Dec 21, 1999 · N819AL · Boeing 73725A · APU Core Engine
Back to Boeing 737-25A