Boeing 757-23A
Service difficulty reports · 1,396
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 = '75723A' 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.
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 = '75723A' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA202608261232Frame · crackedRIGHT, BS 1640 FUSELAGE FRAME WEB AT STRINGER 14R UPPER INBD CRACK INDICATION AT 2:00 O'CLOCK, AROUND THE BOTTOM INBD HOLE WITH TWO CRACK INDICATIONS AT 2:00 O'CLOCK AND 7:00 O'CLOCK FACING AFT. FRAME REPAIRED IAW EA F-5310-T0388261, PART 1, & 2. THIS EA DEVSDR FDEA202608251224Skin Panel · crackedLH WING NR 3 SLAT MAIN TRACK SUPPORT AREA LOWER SURFACE SKIN WITH CRACKED. COVE PANEL WITH CRACK AT LH WING # 3 SLAT MAIN TRACK SUPPORT AREA LOWER SURFACE WAS REMOVED, FABRICATED AND INSTALLED IAW B757 SRM 51-40-02-0G AND B-DWG 114N4077 REV DSDR FDEA202608211211Power Supply · faultedR1 EMERGENCY EXIT LIGHT FAILS OPS TEST. PREMATURE REMOVAL/INSTALLATION OFF MPN: 2012-1. REPLACED BATTERY, NO HELP. REMOVED AND REPLACED POWER SUPPLY/TRAY ASSY AND INSTALLED NEW BATTERY, OPS CHECKS NORMAL. OK TO CONTINUE. CHARGER/TRAY REMOVED P/N 201SDR FDEA202608201198Battery Pack · failedINTERIOR EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED FWD BATTERY POWER SUPPLY IAW ABOVE REF. AFTER REPLACMENT FOUND CTR EXIT LIGHT AND R1 EXIT LIGHT OPS CHK SERVICEABLE. L1 DOOR OVERHEAD EXIT LIGHT AND FLT DECK EMER LIGHT INOP. PRESSED COURIER TEST BUTSDR FDEA202608131118Floorbeam · corrodedMAIN CABIN FLOORBEAM AT BS 1200 BETWEEN BL 0 TO LBL 24.75 WITH CORROSION FLOORBEAM SECTION OUT OF LIMITS AT MAIN CABIN B.S 1200 BETWEEN LBL 5 TO LBL 11 WAS REPAIRED IAW B-757 SRM 53-00-51-2R FIG 201 REPAIR 5.SDR FDEA202608121116Seat Track · corrodedMAIN CABIN SEAT TRACK BEWTEEN BS 1060 TO 1080 RBL 45.50 WITH CORROSION MAIN CABIN SEAT TRACK SUPPORT (UPPER CHORD) BETWEEN STA 1040-1080 WITH CORROSION OUT OF LIMITS IAW B-757 SRM 53-00-52-1A FIG 101 DETAIL VII WAS REMOVED, FABRICATED AND INSTALLED IAW BSDR FDEA202608121115Seat Track · corrodedMAIN CABIN SEAT TRACK BETWEEN BS 1180 TO BS 1200 LBL 24.75 OUTB FLANGE WITH CORROSION REMOVED CORROSION AT MAIN CABIN SEAT TRACK AT STA 1180 TO 1200 LBL 24.75 IAW B757 SRM 51-10-02-0G FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00-52-1A FIG 101 DETAIL VII SDR FDEA202608081101Skin · damagedEVALUATE EXISTING DOUBLER REPAIR ON RH INBOARD MAIN FLAP LOWER SURFACE, NEAR MF STA 147.00 FOR RSC TRACKING PURPOSE ONLY EXISTING REPAIR ON RH INBOARD MAIN FLAP LOWER SURFACE NEAR MF STA 147.00 WAS EVALUATED UNDER FEDEX EA # F-5750-T0388266 A P1 WITH TITSDR FDEA202608081100Skin · damagedEVALUATE EXISTING COMPOSITE REPAIR AT LT ELEVATOR UPPER SURFACE T/E, OUTBOARD AREA. REPAIRED AT LH ELEVATOR UPPER SURFACE T/E, OUTBOARD AREA WAS EVALUATED UNDER E.A.#: F-5520-T0388252 P1.SDR FDEA202607100886Lanyard · out of positionDURING PREFIGHT FOUND R-1 DOOR WILL NOT ARM . DOOR IS LOCKED AND INDICATED. AMM: 25-66-01-4 FOUND R1 PASSENDER DOOR STATIC LINE CAUGHT IN PUSHROD. REROUTED CARBINER STATIC LINE NO DEFECTS NOTED. OPS CHECKED GOOD. ACFT OK FOR SERVICE.SDR FDEA202606240800Unknown · odorAFTER LOWERING MLG THERE WAS A DISTINCT ELECTRICAL BURNING ODOR. EXPERIENCED THIS ABOUT 2 WEEKS AGO ON THIS SAME ACFT. AMM 32-61-00-5 PINNED GEAR & CYCLED GEAR HANDLE WITH HYD APPLIED. ALL INDICATIONS NORMAL IAW AMM, NO ODOR OF OZONE PRESENT. INSPECTED BEHSDR FDEA202605280647Adc · faultedALTITUDE DISAGREE TWO TIMES DURING DESCENT. FO ALTIMETER MATCHED THE STANDBY AND WAS 400 FEET DIFFERENT THAN CAPTAINS AMM: 34-12-01-4 REMOVED AND REPLACED CAPTAINS ADC. GROUND TEST NORMAL. PARTS INPUT WRI 34-16/ 7188. AMM: 34-12-01-4 REMOVED AND RSDR FDEA202605080570Skin · damagedLH OUTBOARD AILERON TRAILING EDGE HAS DAMAGE, MARKED WITH TAPE. REPAIRED DAMAGE ON L/H O/B AILERON AT WS 796.26 IN REF TO B757 SRM 57-60-01-2R FIG 201 SH 2 AND B757 SRM 51-70-05-0G FIG 5. CALCULATED NEW BALANCE MOMENT FOR L/H O/B AILERON TO BE -12.30 POUNDSDR FDEA202604180469Fseu · failedWHILE CONFIGURING FOR LANDING, AS WE SELECTED FLAPS 25, WE RECEIVED A TE FLAPS DISAGREE ON EICAS. INDICATOR REMAINED AT FLAPS 20. COMPLIED WITH QRH. RETRACTED FLAPS USING ALTERNATE METHOD. UNEVENTFUL LANDING IN HNL. EMERGENCY DECLARED. RAN FLAPS THROUGH FSDR FDEA202604030397Skin · dentedR/WING O/B T/E MAIN FLAP LOWER SURFACE HAS A DENT PANEL ASSY SKIN OUTER PLY THIS ITEM HAS BEEN ACCOMPLISHED ON EA F-5750-T0386919.SDR FDEA202604020393Frame · crackedDURING ACCOMPLISHMENT WC EF 530-E0329085 D P6 MAIN FRAME BODY STATION 1640 FUSELAGE FRAME INSPECTION FOUND MISSING INTERNAL STRAP IN FRAME AT BS 640 BETWEEN STR 13R TO STR 17R THIS ITEM HAS BEEN ACCOMPLISHED ON FEDEX EA # F-5310-T0353582 TITLE: "FUSELAGE-SDR FDEA202603220365Skin · corroded#2 ENG. L/H FUSELAGE EXTERIOR COMPOSITE PANEL HAS CORROSION ON OUTER ALUMINUM SKIN AT FWD LWR CORNER NEAR APU PLENUM DRAIN. APPROX. STA. 1904 REF. BOEING DWG. 148N3710. "#2 ENG" LOCATION IS INCORRECT, SEE REMAINDER OF DISCREPANCY REPAIRED L/H FUSELAGE EXTESDR FDEA202603190358Fseu · failedUPON SELECTING FLAPS 25 RECEIVED A TE FLAP DISAGREE EICAS. FLAP HANDLE WAS AT 25 BUT THE FLAPS WERE AT 20. RAN QRH, RETRACTED FLAPS TO UP USING ALT FLAPS AND DIVERTED TO HNL. UNEVENTFUL FLAPS 20 LANDING USING ALT FLAPS. EMERGENCY DECLARED. INTERROGATSDR FDEA202508291579Frame · crackedCRACK INDICATIONS FOUND IN STA 1640 AT S-14R BOTTOM I/B OPEN HOLE APROX AT 8 O' CLOCK LOOKING AFT AND TWO CRACK INDICATIONS IN UPPER O/B OPEN HOLE APROX AT 6 & 7 O' CLOCK LOOKING AFT COMPLIED WITH EA # F-5310-T0384596 P1 TITLE: FUSELAGE -MAINFRAME -STA 16SDR FDEA202508281562Skin · delaminatedLH WING LEADING EDGE SKIN AREA CRACKED BETWEEN WS 150.5 AND 204.50 (#5 LEADING EDGE SLAT AREA ) PERFORMED TAP TEST ON LH WING L/E DELAMINATION FOUND DIM L= 18.5" W=15" OUT OF LIMIT IAW B757 SRM 57-41-01-1A FIG 101 SHEET 2 TABLE I NOTE A AND IAW B757 SRM 5SDR FDEA202507301342Skin · dentedRIGHT HORIZONTAL STAB. UPPER SKIN WITH DENT BETWEEN STAB STA 104.248 AND STA 152.248 AND BETWEEN FRONT . SPAR AND AUX SPAR. EVALUATED DENT ON RH HORIZONTAL STAB UPPER SKIN BETWEEN STAB STA 104.248 - 152.248 AND BETWEEN FRONT SPAR & AUX SPAR FOUND THE FOLLWSDR FDEA202507221293Socket · loosePARKING BRAKE DISCRETE LIGHT DOES NOT ILLUMINATE WHEN PARKING BRAKE SET FOUND PARKING BRAKE LIGHT BASE ASSY LOOSE, TIGHTEN BASE. LIGHT OPS CKED GOOD. A/C OK FOR SERVICE.SDR FDEA202507191267Skin · damagedWHILE PERFORMING INSPECTION ON THE #2 CARGO DOOR LWR CORNERS SKIN CUTOUT FWD AND AFT, FOUND A REPAIR ON THE AFT LOWER CORNER OF THE #2 CARGO DOOR AREA. AD2006-11-11 FUSELAGE PREVIOUS REPAIR AT NO. 2 CARGO DOOR CUTOUT BS 1410-1445 STR 25- 28R. ACCOMPLISHED SSDR FDEA202507141192Floorbeam · corrodedMCD STA 1640 SUPPORT BEAM BL 0.00 TO LBL 45.50 HAS CORROSION. REMOVED CORROSION AT STA 1640 SUPPORT BEAM BL 0.00 - LBL 45050 IAW SRM 51-10-02. FOUND OUT OF LIMIT IAW SRM 53-00-51-1A. REPAIRED FLOOR BEAM AT STA 1640, LBL 45.50 IAW SRM 53- 00-51-2R. MAJOR REPSDR FDEA202507141191Crease Beam · corrodedCORROSION NOTED ON THE ATTACHMENT FRAME OF MAIN DECK FLOORBOARD # 252 MKF (RH MOST O/B) AT STA 1540 - 1620. REPAIRED FRAME ATTACHMENT (CREASE BEAM) AT MAIN CABIN R/H STA 1540 - 1620 IAW SRM 53- 00-13-2R. MAJOR REPAIR.SDR FDEA202507111182Seat Track · corrodedCORROSION NOTED ON THE SEAT TRACK BASE AT LH STA 1200-1240 I/B OF FLOOR PNL 251 MCF. REMOVED AND REPLACED SEAT TRACK AT L/H STA 1180 TO 1240 LBL 45.50 IAW SRM 51-40-02 AND SRM 53-60-52-01. MAJOR REPAIR.SDR FDEA202501270142Lens · detachedL EXTERNAL EMERGENCY LIGHT COVER DETACHED. IAW AMM 33-51-06-2-1 EA TF-3350-T0313211 L EMERG LIGHT LENS REATTACHED IAW SPM AND AMM 33-51-06-2-1 TESTED OK.SDR FDEA202501270140Lens · detachedEXTERNAL LH EMER. LIGHT LENSE DETACHED. L EMERG LIGHT LENS REATTACHED IAW SPM AND AMM 33-51-06-2-1 TESTED OK ADD CLEAREDSDR FDEA202501150070Battery · failedEMERGENCY LIGHTS FOR R1 DOOR AND CENTER COURIER AREA INOP. IAW AMM: 33-51-07-2 REMOVED AND REPLACED BATERYPACK ASSY FOR CHARGER ASSEMBLY M730. OPS CHECK GOOD.SDR FDEA202412021762Guard · damagedEMERGENCY EXIT LIGHTS ARE UNARMED WHEN EMERGENCY EXIT LIGHT SWITCH IS CLOSED. FOUND SWITCH GUARD SPRING LOAD OUTSIDE OF THE SWITCH, REPOSITIONED THE SPRING, PERFORMED EMERGENCY LIGHTS OPERATIONAL IAW AMM 33-51-00-5 TEST OKSDR FDEA202409211334Skin · dentedINCOMING A/C DAMAGE JUST BELOW AND FWD OF THE MAIN CARGO DOOR. DENT MEASURING APPROX 2"X3" AND MAX DEPTH OF 0.0119. LOCATED 2" AFT OF FS460 JUST BELOW STR 18L. FUSELAGE - PLATES AND SKINS - INCOMING DENT DAMAGE FWD OF MAIN CARGO DOOR - DOUBLER REPAIR. ACCOSDR FDEA202409111303Floorboard · damagedMAIN DECK CARGO COMPT FLOORBOARD PANEL 252 MWF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MWF ON VTMAE TRAVELER T24/1774253 IAW DRAWING SRZ-25-005 REVISION R MAJOR REPAIR.SDR FDEA202409111302Floorboard · damagedMAIN DECK CARGO COMPT FLOORBOARD PANEL 251 MWF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MWF ON VTMAE TRAVELER T24/1774230 IAW DRAWING SRZ-25-005 REVISION R MAJOR REPAIR.SDR FDEA202409111301Floorboard · damagedMAIN DECK FLOORGOARD PANEL 251MXF IN ZONE 250 DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MXF ON VTMAE TRAVELER #T24/1774251 IAW SRZ-25-005 REVISION R DRAWING MAJOR REPAIR.SDR FDEA202408081109Skin · corrodedFOUND EXFOLIATION CORROSION ON EXTERIOR SKIN SURFACE ADJACENT TO L/H APY DOOR FWD HINGE POINT AREA COMPLIED WITH MAJOR REPAIR CLASSIFICATION. E.A. #-F-5330-T0380244 P1 FUSELAGE-PLATES AND SKIN- LH APU COMPARTMENT SKIN PANEL REPAIR BETWEEN STA. 1885.20 AND SDR FDEA202407251057Relay · failedNOSE L/G COMPONENTS INSPECTION REQUIRED TO CONFIRM NO DAMAGES. NOSE GEAR COMPONENTS VISUAL INSPECTION PERFORMED. NO OBVIOUS DAMAGES OBSERVED. ALSO NOSE GEAR STEERING OPERATIONAL TEST PERFORMED SATIS REF AMM 32-51-00-5-3.SDR FDEA202407251056Relay · failedRUNWAY ENGINE START. INSTEAD OF STABILIZING AT IDLE, THE RPM AND THRUST INCREASED WITH NO THROTTLE INPUT AND THROTTLES AT IDLE AND CONTINUED TO INCREASE RAPIDLY UNTIL CREW CUTOFF FUEL. SLIGHTLY PUSHED THE TUG. EVERYONE IS OK. APPLIED AND IDLE CONTROL RELASDR FDEA202407211036Battery Pack · no testON SERVICE CHECK FOUND EMERGENCY EXIT AISLE SIGN NOT ILLUMINATING WHEN EMERGENCY LIGHTS TEST PERFORMED. AMM: 33-51-07-2-0, REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK AS PER 757 AMM 33-51-07-2-0. OPS CHECK GOOD. AIRCRAFT OK FOR SERSDR FDEA202406230855Battery Pack · failedDURING SVC FOUND THE L1 INSIDE AND OUT EMERGENCY LIGHTS WERE INOP. REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTERY PACK AS REQUIRED IAW AMM 33-51-07-2. OPS CHECK GOOD.SDR FDEA202406010758Support · damagedL/H WING, AFT FAIRING SUPPORT INBD MAIN FLAP FITTING IS LOOSE. FOUND AFT MOUNT HOLE DAMAGED IN LH I/B LWR MAIN FLAP FOR FAIRING SUPPORT BRACKET. REPAIRED DAMAGED HOLE AND REPLACED BRACKET REF. B757 SRM 57-53-02-2R REPAIR 3. AND INSTALLED FAIRING TO BRACKET RSDR FDEA202405250726Controller · failedAT FL400 CABIN ALT HIGH WARNING DONNED MASKS. RAN QRH. INITIATED EMERGENCY DESCENT. CABIN ALTITUDE RATE REACHED 2000 FT PER MIN DOWN AND HIGHEST ALTITUDE REACHED WAS 15 K. EMERGENCY DECLARED AMM: 21-31-02-4, AMM: 21-31-00-5, AMM: 05-51-24-2, CABIN PRESDR FDEA202404300520Fan · failedOIL BURNING SMOKE BELOW 5000FEET WITH LOW POWER SETTING. R & R L/H RECIRCULATION FILTER AND FAN, REVERSED MEL 21-25-01-02 & MEL 21-58-07, RECONNECTED WIRE ON PLUG D40910J, PERFORMED LT RECIRCULATION FAN & EQUIPMENT COOLING TEST, ALL TESTS PASSED, LEAK CHECSDR FDEA202404230272Girt Bar · out of alignmentLIGHT ON LEFT CREW ENTRY DOOR INOP. FACT 23APR24 08:51 AMS AMM: 25-66-10-2 AMM: 25-66-11-2 RELAMP NO HELP. FOUND SLIDE VERY HARD TO ARM AND GIRTBAR FITTINGS NOT REACHING THE TARGETS. RE-INSTALLED GIRTBAR FLAP AS PER AMM 25-66-10-2 REV 133.9 VERIFEDSDR FDEA202404030435Lamp · burned outL1 MAIN ENTRY DOOR SLIDE LIGHT IS BURNT OUT. REMOVED AND REPLACED BOTH BULBS AND PERFORMED ADJUSTMENT TEST IAW AMM 52-11-00-2-0, TEST SATIS, A/C OK FOR SERVICE.SDR FDEA202404010430Skin · corrodedR / WING DRY BAY ACCESS PANEL 644AB WING NUT PLATES DAMAGED WITH POSSIBLE EXFOLIATION ON WING SKIN. COMPLIED WITH EA F-5730-T0378521 P1 WINGS-PLATE AND SKIN CORROSION R/H WING LOWER DRY BAY PANEL REPAIR AT ACCESS PANEL CUTOUT 644 AB, WS 775-806 WITH NO DEVSDR FDEA202403290410Web · corrodedFWD CARGO COMPARTMENT F. STA BETWEEN 600-620 RBL 64.5 SHEAR WEB HAS CORROSION AFTER EVALUATED SHEAR WEB AT F.STA 600 TO 620 AND BTW RBL 62.89 - 64.5 FOUND OUT OF LIMITS IAW B-757 SRM 53-30-13-1A FIG 101 DETAIL III ; REMOVED, FABRICATED AND INSSDR FDEA202403290408Fairing · gougedSEC 48 F.ST 1862.2 S.14BL HAS TYPICAL GOUGE CAUSED BY STAB BLADE SEAL L/H CLEANED GOUGED AREA ON TWO DIFERENT PARTS AFFECTED ( PANEL FAIRING) IAW B-SOPM 20-30-03 AND AFTER EVALUATION TWO DIFERENT AREAS FOUND # 1 AREA AT STA 1862 TO STA 1865 FOUND WITHISDR FDEA202403280399Seat Track · corrodedMAIN CABIN FOUND CORROSION ON SEAT TRACK STA 1180-1200 RBL45.50 REMOVED CORROSION AT SEAT TRACK FLANGE BETWEEN STA. 1180-1200 RBL 45.50, EVALUATED AREA FOUND TO BE OUT OF LIMITS IAW B 757 SRM 53-00-52-1A FIG. 101 DETAIL VIII REMOVED AND INSTALLED NEW SEAT SDR FDEA202403280391Window · crackedWHILE IN CRUISE FLIGHT FL360, CAPTAIN SIDE FRONT WINDSCREEN ARCED FOLLOWED BY SHATTERING WITH OUTER PAIN. RAN QRH, ARCING CONTINUED. POSSIBLE DEFORMED WINDOW WITH CONTINUING ARCING THROUGHOUT DESCENT. EMERGENCY DECLARED. REMOVED & REPLACED L1 WINDOW AS PER SDR FDEA202403270388Seat Track · corrodedSEAT TRACK HAS EVIDENCE OF CORROSION ALONG FLANGE UNDER CRACKED PAINT BETWEEN STA 1320-1420 RBL-44 REMOVED CORROSION AT SEAT TRACK I\B FLANGE BETWEEN STA 1320-1420 RBL44 IAW B757 SRM 51-10-02-0G, EVALUATED AREAS FOUND TO BE OUT OF LIMITS IAW B757 SRM 53-00
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