Boeing 757-23A
Service difficulty reports · 1,397
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 FDEA202209292386Light · looseDURING PREFLIGHT UNARMED LIGHT CAME OUT OF EMERGENCY LIGHTS MODULE ON OVERHEAD PANEL FOUND KORRY LIGHT ASSY BROKEN. R&R KORRY ASSY IAW AMM 33-13-00-2 AND SWPM 20-84-18. OPS CHECK SATIS. A/C OK TO CONTINUE.SDR FDEA202209052207Socket · failedAT BLOCK IN THE SLIDE ARM LIGHT ON DOOR L1 IS BURNT OUT. SERVICED L1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT WITH NEW BULB WITH NO HELP. TRIED WITH THE LENS & BULB HOLDER OF THE OTHER SIDE WITH NO HELP. CONFIRMED GOOD ADJUSTEMENT OF THE GIRT BAR & ITS ASSOSDR FDEA202208302101Control Valve · faultedRIGHT PACK OVERTEMP AND FAILED INFLIGHT. LEFT WAS MEL ED,DESCENDED BELOW 10000 ON OXYGEN. EMERGENCY DECLARED. AMM21-51-00-5, FIM21-51 TREE 803, 805. PERFORMED OPS TEST OF RH PACK AND CONTROL SYSTEM, AND BITE CHECKS OF CONTROLLERS. NO FAILURES OR MALFUNSDR FDEA202206251551Oil System · low pressureLEFT ENGINE OIL QUANTITY DECREASED TO 0 ON TAKEOFF, PRESSURE DECREASED TO 0 AS WELL. L ENG OIL PRESS EICAS MESSAGE ILLUMINATED. RAN QRH AND SHUT DOWN LEFT ENGINE INFLIGHT. LANDED RNO 34L WITHOUT FURTHER INCIDENT. EMERGENCY DECLARED. REMOVED #1 ENGINE RESDR FDEA202205101167Girt Bar · dirtyPDIS 938 25-60 8387 10MAY22 SJO FACT U ENTRY DOOR KNUCKLE BUSTER WILL NOT DEPLOY WHEN ARMING DOOR. FACT 10MAY22 01:43 SJO U INSPECTED L1 ENTRY DOOR AND REMOVED DEBRIS FROM GIRT BAR , PERFORMED OPS CK IAW AMM 25-66-10-2. ALL CKS NORMSDR FDEA202201060169Seat Track · corrodedSTA 480-620, LBL 45.50, FOUND CORROSION ON SEAT TRACK WORK ACCOMPLISHED IN ACCORDANCE WITH EO #F-5310-T0366384. MAJOR REPAIR.SDR FDEA202111222974Skin · damagedFUSELAGE BELLY SKIN AT BS 1460 TO 1480 BETWEEN STRINGER 29L AND 29R THERE IS A DOUBLER AND A TRIPLER INSTALLED UNDER THE VHF ANTENAN. REPAIR REQUIRES EVALUATION TO DETERMINE IF IT WAS ACCOMPLISHED IN ACCORDANCE WITH APPROVED DATA A DVI WAS PERFORMED PESDR FDEA202111182976Skin · damagedEMPENNAGE , TAIL CONE UPPER SURFACE LEFT HAND SIDE , CIRCULAR DUBLER REPAIR ON EXTERNAL SKIN FORWARD OF THE APU EXHAUST OUTLET AT BS 1980, REPAIR REQUIRES EVALUATION TO DETERMINE IF IT WAS ACCOMPLISHED IN ACCORDANCE WITH APPROVED DATA PERFORMED DVI PER SSDR FDEA202111182975Skin · damagedAPU COMPARTMENT R/H SIDE , CIRCULAR DOUBLER REPAIR ON INNER SKIN AT BS 1925 AND INCHES FROM THE PANEL LOWER EDGE REPAIR REQUIRES EVALUATION TO DETERMINE IF IT WAS ACCOMPLISHED IN ACCORDANCE WITH APPROVED DATA PERFORMED DVI PER SRM 51-10-08. REPAIR EVALUASDR FDEA202110252971Floorbeam · corrodedFOUND CORROSION ON STA 1640 ON UPPER CHORD OF FLOOR BEAM BETWEEN LBL 45 TO RBL 45 THE CORREDED UPPER CHORD WAS REMOVED AND DISCARDED A NEW REPAIR UPPER CHORD P/N FX-F-5310-T036209-01 WAS INSTALLED PER EA # F-5310-T036209 P1 USING FASTENERS PER SRM 51-40-SDR FDEA202110242977Wedge · damagedDURING C-DUCT REMOVEL R/H INBD L/H SLAT DAMAGED PERFORMED REPAIR PER EA F-5750-T0365723A REP DIM. 5.2" X 7" REP. LOC. ISS 137 AT T/E. PERFORMED HOT BOND REPAIR PER SRM 51-70-10 , REF SRM 57-43-02-2R, FIG 201 DETAIL II, NOTE D, TABLE 201SDR FDEA202108262107Handle · unsecureDURING A TEST FLIGHT, LT ENTRU DOOR EICAS MSG, IMMEDIATELY AFTER TAKEOFF. HANDLE HAD POPPED UP APPROX 6 INCHES AND WOULD NOT LOCK BACK DOWN. NO ABNORMAL PRESSURIZATION ISSUES. ADJUSTED THE L1 DOOR IAW AMM 52-11-00, OPS CHECKED GOOD.SDR FDEA202108232075Handle · unsecureTEST FLIGHT- L FWD ENT DOOR EICAS OCCURRED IN THE APPROACH PATTERN. THE DOOR HANDLE HAD POPPED UP APPROX 6 IN. FROM FULL LOCKED POSITION. COULD MOVE HANDLE DOWN ENOUGH TO EXTINGUISH LIGHT BUT NOT ENOUGH TO OVER-CENTER AND LOCK DOOR. REMOVED L-1 LINING DOORSDR FDEA202108192042Frame · crackedL/H SIDE FR 1640 S-14 WEB FRAME. BOTH BOTTOM INBD AND OUTBD HOLES HAVE CRACK INDICATIONS. CLOCK POSITION FOR BOTH HOLES ARE 9 AND 3:00 O'CLOCK. ACCOMPLISHED FINAL EA F-5310-T0362919 FUSELAGE - MAIN FRAME - STA 1640 FRAME SPLICE REPAIR BETWEEN STRINGER I-9SDR FDEA202108172021Light · inoperativeMDIS 922 33-50 2242 13AUG21 CDG FACT U FOUND L1 EMER DOOR GROUND ILLUMINATION LIGHT INOP. SHGN 13AUG21 19:28 CDG U RELAMPED AS PER MM:33-51-06-2-1. LIGHT TEST OK. DURING L1 EMER LIGHT LENS REINSTALLATION, FOUND 4 SCREWS WORN AND UNABLE TOSDR FDEA202108102000Floor Panel · crackedMAIN DECK FLOOR PANEL 251MWF HAS CRACK (ADAJACENT L4 DOOR) DOT 136-51 FABRICATED MAIN DECK PANEL 251MWF ON VTMAE TRAVELER # T21/1565104 IAW DWG SRZ-25- 005 REVISION R, MAJOR REPAIR.SDR FDEA202108051998Bulb · inoperativeEMERGENCY LIGHT DOOR 1L (SLIDE GND ILLUMINATION LT) INOP BULB REPLACED ACC AMM 33-51-06-2-1 REV 124.17. OPS TEST SATIS.SDR FDEA202107271872Door · crackedLMG BODY DOOR CRACKED AFT OF TANG REPAIRED LMG DOOR CRACKED AFT OF TANG IAW FEDEX B757 SRM: 52-80-02, 51-70-06-0G, DWG #149N6003 AND AMM 51-21-00. MINOR REPAIRSDR FDEA202106291620Sensor · dirtyL1 DOOR SLIDE LIGHT INOP UPON LANDING. DOOR 1L GIRT BAR FITTINGS, SLIDER AND PROXIMITY SENSOR CLEANED FROM DEBRIS. GIRT BAR CYCLED SEVERAL TIMES AND SLIDE ARMED INDICATION LIGHT CHECKED IAW AMM 25-66-00-0-4.SDR FDEA202106111497Bulb · inoperativeDOOR 1L SLIDE ARM LIGHT INTERMITTENT, MOSTLY INOP LH SLIDE ARMED INDICATOR LIGHT BOTH BULBS REPLACED IAW SWPM 20-84-18 IAW AMM 52-11-00, LH SLIDE HAS BEEN ARMED AND DISARMED SEVERAL TIMES IN ORDER TO CHECK GOOD FUNCTIONING OF THE LH "SLIDE" ARMED INDICSDR FDEA202105281418Controller · malfunctionedDURING CLIMB COCKPIT TEMP BECAME EXCESSIVELY HOT. RAN QRH AND AFTER TRIM AIR SWITCH TURNED OFF REGAINED TEMP CONTROL. PERFORMED BITE TEST ON CABIN ZONE TEMP CONTROLLER. NO CURRENT FAULTS OR PREVIOUS FAULTS NOTED. REMOVED AND REPLACED CABIN ZONE TEMP CONTSDR FDEA202105261402Bulb · inoperativePDIS 920 25-60 2709 26MAY21 CDG OPEN U LOGPAGES:3001081 1L SLIDE ARMED LIGHT DID NOT ILLUMINATE WHEN ARMED RELEASED FOR SERVICE PER MEL : 25-66-05-A CATEGORY : C EXPIRATION : 05JUN21 "MEL 25-66-05-A: L1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGSDR FDEA202105201334Girt Bar · disengagedWHEN OPENING R1 DOOR NOTED GIRT BAR HANGING DOWN FROM BOTTOM OF DOOR. COMPLIED WITH B757 AMM 25-66-10-2 PAGES 14-15 STEPS 14-21. RENEGAGED THE GIRT BAR CAMS IN THE SDR FDEA202105051128Seat Track · corrodedDOT# 106-12, MAIN CARGO COMPT APPROX. STA. 1340, RBL 45.50 SEAT TRACK HAS CORROSION. CUT OUT DAMAGE SEAT TRACK FROM STA 1300 TO STA 1350 RBL 45.5 IAW SRM 53-00-52-2R, REPAIR SEAT TRACK IAW SRM 53-00-52-2R. (INSTALLED NEW SEAT TRACK SECTION) MAJOR REPAIR.SDR FDEA202105051119Floor Panel · delaminatedCOURIER FLOOR PANEL 221BF DELAMINATED. FABRICATED COURIER FLOOR PANEL 221BF ON VTMAE TRAVELER #T21/1548308 IAW FEDEX DWG. DWG. NO. SRZ-25-005 REV. R CAT "A" MAJOR REPAIR.SDR FDEA202105051118Floor Panel · delaminatedCOURIER FLOOR PANEL 221AF DELAMINATED. FABRICATED COURIER FLOOR PANEL 221AF ON VTMAE TRAVELER #T21/1548307 IAW FEDEX DWG DWG NO. SRZ-25-005 REV R. CAT "A" MAJOR REPAIR.SDR FDEA202105051117Floor Panel · delaminatedCOURIER FLOOR PANEL 222MAF DELAMINATED. FABRICATED FLOOR PANEL 222MAF ON VTMAE TRAVELER #T21/1548305 IAW DWG SRZ-25-005 REV REV R CAT "A" MAJOR REPAIR.SDR FDEA202105051116Floor Panel · delaminatedCOURIER FLOOR PANEL 221MBF DELAMINATED. FABRICATED COURIER FLOOR PANEL 221MBF ON VTMAE TRAVELER #T21/1548304 IAW DWG SRZ- SRZ-25-005 REV R CAT "A" MAJOR REPAIR.SDR FDEA202105051114Floor Panel · delaminatedCOURIER 222AF FLOOR PANEL DELAMINATED. FABRICATED 222AF COURIER FLOOR PANEL ON VTMAE TRAVELER #T21/1548306 IAW DWG SRZ-25- SRZ-25-005 REV R, CAT "A" MAJOR REPAIR.SDR FDEA202104210963Case · corrodedENGINE #1 LP COMPRESSOR FRONT CASE OUTER SURFACE FORWARD OF KEVLAR WRAPPING IS CORRODED FROM 4 O'CLOCK TO 12 O'CLOCK POSITION (AFT LOOKING FORWARD) SNRM RECTIFIED AS PART OF ESN 30690 REMOVAL AND INSTALLATION OF ESN 30775 AS PER WO 79687 SEQ: 000235SDR FDEA202104010808Valve · failedLEFT ENGINE WOULD NOT SHUTDOWN WHEN FUEL CUTOFF MOVED TO CUTOFF. IT RAN FOR APPROXIMATELY 25 SECONDS BEFORE SHUTTING DOWN. REMOVED L/H ENGINE FUEL FLOW GOVERNOR AS PER AMM 73-21-01-4-4. INSTALLED LEFT ENG FFG IAW AMM 73-21-01-4-4. PERFORMED ENG LEAK CHECSDR FDEA202103060583Plug · looseAT CRUISE AT FL350 THE RIGHT AND TOTAL QTY INDICATIONS ARE INTERMITTENT. AT OTHER TIMES THE RIGHT QTY INDICATION FLUTUATED - 1,000 POUNDS. DIVERTED TO SIN AND MX APPLIED MEL 28-41-01-01/28-41-07-A FOUND M723 BUSSING PLUG UNIT WAS LOOSEN, RETIGHTENED THE SDR FDEA202102050296Apu · odorPDIS 939 21-70 8622 05FEB21 LGG OPEN U LOGPAGES:3301364 OBSERVED AN ACRID, BURNING OIL SMELL DURING ALL PHASES OF FLIGHT WITH MARKED INTENSITY ON APU BLEED, CLIMB AND DESCENTS. EXPIRIENCED WHAT IS DESCRIBED AS A FUME EVENT. SHGN 05FEB21 01:2SDR FDEA202101130073Lock · looseLEFT FWD ENTRY DOOR GIRT BAR IS LOOSE AND NEEDS TO BE RESTOWED. REINSTALLED L/H DOOR GIRT BAR AND GIRT BAR SLIDER WITH HIS PROX SWITCH TARGET AS PER AMM 25-66-10-2. TESTED AS PER SAME AMM, TEST PASSED.SDR FDEA202101090053Test Switch · looseEMERGENCY LIGHT TEST SWITCH ABOVE DOOR 1L DOES NOT ILLUMINATE WHEN PUSHED AND EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN TEST SWITCH PUSHED. IDENTIFIED PARTS SWITCH ASSEMBLY. FOUND WIRE AT NO CONNECTION AT SWITCH S10292 LOOSE. RECONNECTED AND FUNCTION TESTED, SDR FDEA202012313226Actuator · malfunctionedGEAR DISAGREE WHEN LANDING GEAR LEVER SELECTED DOWN BEFORE LANDING. NOSE GEAR INDICATED UNSAFE. RAN QRH FOR GEAR DISAGREE AND EXTENDED GEAR VIA ALTERNATE EXTENSION. EMERGENCY DECLARED. REMOVED AND REPLACED NOSE LANDING GEAR LOCKING ACTUATOR, REF B757 AMM 3SDR FDEA202012243205Gate · corrodedL1 DOOR LOWER GATE LOWER EDGE PITTED ACCOMPLISHED EA NR F-5210-T0358769. DOORS-PASSENGER/CREW-NR 1 PASS, DOOR LOWER GATE, EDGE PITTING.SDR FDEA202012223200Shelf · crackedE&E COMPARTMENT E3-2 SHELF LT OUTBOARD MOUNT BRACKET CRACKED, REPAIRED PER SRZ-53-007.SDR FDEA202012223199Mount · crackedE&E COMPARTMENT E3-1 SHELF LT OUTBOARD MOUNT BRACKET CRACKED, REPAIRED PER SRZ-53-007.SDR FDEA202012223197Flange · crackedE&E COMPARTMENT E3-2 SHELF LT OUTBOARD MOUNT FLANGE CRACKED. REMOVED AND REPLACED FLANGE, IAW B SRM 51-40-02 AND DWG NR 284N1028 REV C.SDR FDEA202012173180Skin · crackedNOSE WHEEL WELL RT DOOR CUT OUT UPPER SKIN STRIP IS CRACKED AT BS 324 RBL 19. REMOVED AND REPLACED STRIP, PER DWG 141N0094.SDR FDEA202012163169Handle · malfunctionedLEFT MAIN DOOR ARM HANDLE WILL NOT MOVE, REF FIM 52-11 TREE 802. INSPECTED DOOR LATCHING MECHANISMS FOR DEFECTS OR OBSTRUCTIONS WITH NONE FOUND. ALSO, OPERATED L1 DOOR FROM ARM/DISARM WITH SLIDE REMOVED, PER MEL WITH NO BINDING OR DEFECTS NOTED. REMAINS ON SDR FDEA202011102805Actuator · failedPDIS 994 32-30 8627 10NOV20 IND OPEN U. GEAR DISAGREE AND GEAR DOORS EICAS FOR 90 SECONDS UNTIL GEAR FULLY RETRACTED AND EICAS MESSAGES. NOISE FROM NOSE GEAR AREA UNTIL DOORS MESSAGES WENT AWAY. REPEAT WRITE UP. SHGN 10NOV20 06:12 IND U. CREW REPORTED THASDR FDEA202010282669Spar · corrodedRIGHT HAND WING LEFT HAND TRAILING EDGE OUTBOARD MAIN FLAP REAR SPAR UPPER CHORD FOUND CORROSION AT AROUND WBL 387 OUTBOARD OF NR 7 FLAP TRACK. EA F-5750-T0357675 COMPLIED WITH. THIS REPAIR CLASSIFIED AS MINOR, AS PER GMM 6-2-100.SDR FDEA202010262652Seat Track · corrodedMAIN DECK, CARGO SEAT TRACK FOUND CORROSION AT STATION 876, RBL 45.5 MAIN DECK STATION 876 RBL 45.5. CARGO SEAT TRACK CORROSION REPAIRED, AS PER B757 SRM 53-00-52-2R REPAIR 1 FIGURE 201. THIS REPAIR CLASSIFIED AS MAJOR, AS PER GMM 6-2-100.SDR FDEA202010122531Panel · delaminatedDELAMINATION FOUND ON RT HORIZ STAB UPPER PANEL, FWD TORQUE BOX UPPER INBOARD PANEL. PERFORMED A CATEGORY C REPAIR, RESIN INJECTION TO UPPER SUFACE OF RT HORIZ STAB INBOARD PANEL 22" FORM INBOARD EDGE, 5" FROM FWD EDGE, IAW SRM 51-70-10 REPAIR 5.SDR FDEA202010042415Controller · malfunctionedAIRCRAFT DID NOT PRESSURIZE DURING CLIMB OUT IN AUTO 2 . LEVELED AT 10K WITH CABIN ALT EICAS WARNING. OUTFLOW VALVE INDICATED FULL OPEN . NO OTHER INDICATIONS ON EICAS. ACCOMPLISHED FIM 21-30 FT 815 AND FIM 21-3- FT 802 BOCK 1 FOUND CASDR FDEA202010042416Controller · failedAIRCRAFT DID NOT PRESSURIZE DURING CLIMB OUT IN AUTO 2. LEVELED AT 10K WITH CABIN ALT EICAS WARNING. OUTFLOW VALVE INDICATED FULL OPEN. NO OTHER INDICATIONS ON EICAS. ACCOMPLISHED FIM 21-30 FT 815 AND FIM 21-3- FT 802 BLOCK 1 FOUND CABIN ALT PRESS CONTROLLSDR FDEA202009232318Landing Gear · failedPDIS 921 32-51 8989 23SEP20 IND OPEN U. AIRCRAFT STILL PULLS HARD TO THE RIGHT. IT TAKES ALMOST 1/2 RUDDER DEFLECTION TO TRACK STRAIGHT. ALSO IT TAKES CONSIDERABLY MORE POWER TO BREAKAWAY AND GET THE JET MOVING, APPROXIMATELY 35% N1 W/BOTH ENGINES. REMOVEDSDR FDEA202009142212Mechanism · brokenDURING PRE-FLIGHT CHECK, FLIGHT CREW NOTE L1 DOOR MECHANISM IS BROKEN. REMOVED AND REPLACED COLLAR ASSY FROM THE L1 DOOR MECHANISM PER AMM 52-11-08-8. OPENED AND CLOSED THE L1 DOOR PER AMM 52-11-00-2 ,OPS TEST OK. A/C OK FOR SERVICE.
Back to Boeing 757-23A