Boeing 757-222
Service difficulty reports · 15,539
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 = '757222' 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 = '757222' 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 FDEA202110062472None · crackedPDIS 789 29-02 4718 05OCT21 MEM OPEN U DURING CRUISE THE C HYD ELEC 2 EICAS MESSAGE APPEARED FOLLOWED BY A COMPLETE REDUCTION OF C HYDRAULIC QUANTITY. SHORTLY AFTER THE FOLLOWING EICAS MESSAGES APPEARED: C HYD SYS PRESS C HYD RSVR PRES C HYD SDR FDEA202110052469Frame · crackedRH 1640 FUSELAGE FRAME WEB AND STR 14 LOWER INBD HOLE HAS CRACK INDICATIONS AT 3 AND 9 O'CLOCK POSITION,, VIEWED LOOKING AFT. COMPLIED WITH FUSELAGE - MAINFRAME - STA 1640 FRAME SPLICE REPAIR TO REPLACE CRACK AT ST-14 RIGHT. EA# F-5310-T0363945. MAJOR REPSDR FDEA202109092264Skin · delaminatedEXISTING REPAIR FOUND DURING AGING AIRCRAFT INSPECTION ON LEFT WING MAIN FLAP LOWER SURFACE, FOUND REPAIR TO BE DELAMINATED. REPAIRED LEFT WING MAIN INBOARD FLAP IAW B757 SRM 57-53-01-2R FIG. 201 AND B757 SRM 51-70-10- 2R REPAIR 4.SDR FDEA202109082248Slide · unwanted deployWHILE WORKING EO F-5200-E0320318 D PT2 L1 DOOR SLIDE DEPLOYED. RELEASED FOR SERVICE. L1 SLIDE MISSING. SLIDE STOWED BEHIND RCB DOOR BOTTLE WILL REQUIRE SERVICING. REMOVED AND REPLACED L1 DOOR SLIDE REF AMM 25-66-00-2.SDR FDEA202109082251Skin · damagedRW #7 SLAT UPPER INBD T/E SURFACE HAS DAMAGE REPAIRED RIGHT WING #7 SLAT IAW FEDEX EA# F-5750-T0363944-P1 WINGS - FLIGHT SURFACES - #7 SLAT - TRAILING EDGE WEDGE - UPPER SKIN - SRM REPAIR DEVIATIONSDR FDEA202109082250Skin · dentedRW #6 SLAT OTBD UPPER T/E SURFACE HAS A DENT REPAIRED RW #6 SLAT O/B UPPER T/E SURFACE IAW B757-SRM 57-43-02-2R FIG. 201 & 51-70-10- 2R REPAIR 4 & FEDEX EA NO. F-5750-T0363939 P1 WINGS - FLIGHT SURFACES - #6 SLAT - TRAILING EDGE WEDGE - UPPER SKIN - SRM RSDR FDEA202109042212Controller · malfunctionedPDIS 791 21-30 4670 04SEP21 CPR OPEN U CABIN ALTITUDE WARNING OCCURRED AT CRUISE FL 390 WITH CABIN ALTITUDE CONTROL IN AUTO 2. BEGAN AN IMMEDIATE EMERGENCY DESCENT TO 16,000 WHILE RUNNING QRC AND QRH CHECKLISTS. CABIN ALTITUDE SEEMED TO COME SDR FDEA202109032192Skin · wornLEFT WING OUTBOARD FLAP, OUTBOARD LEADING EDGE WORN. REPAIRED LEADING EDGE SECTION IAW B757 SRM 57-53-01-2R.SDR FDEA202109022187Hub · crackedRO DOOR, INNER HUB ASSY CRACKED REMOVED & REPLACED HUB ASSY IAW B757 AMM 52-11-13-2SDR FDEA202109022185Skin · debondedL/H WING, INBD FWD FLAP, LOWER INBD T/E SURFACE, EXISTING REPAIR IS DIS-BONDING FROM THE SURFACE OF THE FLAP. REPAIRED L/W INBD FWD FLAP, LOWER INBD T.E. SURFACE BY REMOVING EXISTING DISBOND REPAIR AND INSTALLING NEW IAW B757 SRM 57-53-01-2R FIG 201 SHEET1SDR FDEA202108302165Floor Panel · delaminatedMAIN DECK FLOOR PANEL 221MBF IS DAMAGED ON THE UPPER SURFACE FABRICATED NEW FLOOR PANEL IAW DRAWING SRZ-25-005, REV RSDR FDEA2021083082127Window · sparksDURING PREFLIGHT, SELECTED WINDOW HEAT SWITCHED ON AND IMMEDIATELY HAD RIGHT SIDE WINDOW PRODUCE LARGE SPARK AND AND BEGIN SMOKING. WINDOW SPIRAL HEAT CORD AND TEST WINDOW HEAT, BOTH ACCOMPLISHED, ALSO REF AMM 30-41-00-5 FOR WINDOW HEAT TEST OK.SDR FDEA202108182031Actuator · faultedON CLIMB OUT GOT EICAS MESSAGE LE SLAT DISAGREE AND LEADING EDGE DISCRETE LIGHT RETRACTING THE FLAPS AT 200 KNOTS AND 3000 FEET QRH COMPLIED WITH. TROUBLESHOT PER B757 FIM 27-81 FAULT TREE 803 AND FOUND OVERLOAD INDICATOR TRIPPED ON THE INBD SLAT PDU TORQUE LSDR FDEA202108172026Slide · inoperativeWHEN CLOSING MAIN CABIN DOOR, SLIDE BLEW DOOR OPEN, BUT THE SLIDE DID NOT DEPLOY. REMOVED AND REPLACED L1 PASSENGER DOOR ESCAPE SLIDE. REF 757 MM 25-66-01-4.SDR FDEA202108172044Slide · malfunctionedWHEN CLOSING MAIN CABIN DOOR, SLIDE BLEW DOOR OPEN BUT THE SLIDE DID NOT DEPLOY. REMOVED AND REPLACED L1 PASSENGER DOOR ESCAPE SLIDE. REF 757 MM 25-66-01-4.SDR FDEA202107291889Slide · detachedWITH THE R2 DOOR IN THE DISARMED POSITION, THE SLIDE/ RAFT FELL OUT OF THE DOOR BUT DID NOT INFLATE. THE GIRD BAR REMAINED ATTACHED TO THE AIRCRAFT EVEN THOUGHT THE DOOR WAS DISARMED. R&R R1 DOOR SLIDE IAW B757 AMM 25-66-01-4.SDR FDEA202107281885Indicator · brokenRIGHT MAIN GEAR INDICATION NOT ILLUMINATING. TRIED TO RELAMP AND FOUND RIGHT INDICATOR WAS BROKEN. NO GEAR DISAGREE INDICATION. R/R RIGHT (GREEN) GEAR INDICATOR ASSY - KORRY MPN 434-674-1033-2207 (CPN 3312068 T/L ZERO) IAW AMM 33-16-02-2, OPS GOOD.SDR FDEA202107271871Slide · detachedWITH THE R2 (UPDATED TO REFLECT R1) DOOR IN THE DISARMED POSITION, THE SLIDE/ RAFT FELL OUT OF THE DOOR BUT DID NOT INFLATE. THE GIRT BAR REMAINED ATTACHED TO THE AIRCRAFT EVEN THOUGHT THE DOOR WAS DISARMED. R & R DOOR ESCAPE SLIDE IAW AMM 25-66-01-4, ASSISDR FDEA202107141778Floorboard · damagedMAIN DECK FLOOR PANEL 251MVF (RH) HAS BROKEN CORNER. FABRICATED NEW PANEL IAW FED EX SRZ 25-005 REV RSDR FDEA202107141777Floorboard · damagedMAIN DECK FLOOR PANEL 251MFW(LH) HAS BROKEN CORNER. FABRICATED NEW PANEL IAW FED EX SRZ 25-005-REV RSDR FDEA202107131767Plate · crackedRIGHT WING LEADING EDGE FUELING ACCESS PANEL, DOOR SWITH PLATE IS CRACKED FABRICATED & REPLACED NEW CLIP IAW BAC DWG 284N1138 REV -SDR FDEA202107131763Doubler · chafedEXISTING REPAIR DOUBLER AT STA 1862 - 1875, S-17L IS CHAFED. REMOVED & REPLACED REPAIR DOUBLER IAW B757 SRM 53-80-01-2R, FIGURE 201, REPAIR 2SDR FDEA202107121751Skin · chafedRH FUSELAGE @ STA 1862.7 - 1875, S-17R, EXISTING DOUBLER HAS CHAFING DAMAGE ON EXTERIOR SURFACE REMOVED & REPLACED REPAIR DOUBLER IAW B757 SRM 53-80-01-2R, FIGURE 201, REPAIR 2SDR FDEA202107091712Skin · crackedLEFT WING FIXED LEADING EDGE SKIN IS CRACKED @ FSS 360 REPAIRED LEADING EDGE SKIN IAW B757 SRM 57-41-01. LEADING EDGE SKIN REMOVED & REINSTALLED FOR ACCESS IAW B757 SRM 51-40-02-0G & BAC DWG 114N2035 REV -SDR FDEA202107091711Skin · crackedLEFT WING, FIXED LEADING EDGE SKIN @ FSS 550 IS CRACKED REPAIRED LEADING EDGE SKIN IAW B757 SRM 57-41-01, FIGURE 201. LEADING EDGE SKIN REMOVED & REINSTALLED FOR ACCESS IAW B757 SRM 51-40-02-0G & BAC DWG 114N2035 REV -.SDR FDEA202107051687Bracket · crackedFWD LOWER CARGO DOOR AFT UPPER INTERIOR CORNER IS CRACKED REMOVED AND REPLACED FWD CARGO DOOR AFT INTERIOR CORNER IAW BAC DWG 143N6603 REV:F AND B757 SRM 51-40-02SDR FDEA202107031662Collar · crackedDURING SERVICE CHK FOUND 1R DOOR HOLD OPEN LOCK BROKEN. RMVD AND RPLD R1 DOOR HOLD-OPEN LOCK- DOOR HOLD OPEN LOCK CHKS GOOD- REF: B757 M/M 52-11-08-8SDR FDEA202106291613None · noneL1 DOOR SLIDE LIGHT IS INOPERATIVE. REF AMM 33-51-06-2-1, RELAMPED L1 DOOR SLIDE LIGHT. NO HELP. RELEASED FOR SERVICE PER MEL 33-51-02-02. TROUBLESHOT L1 DOOR SLIDE LIGHT IAW 757 FIM 33-51 FAULT TREE 803. NO FAULTS NOTED.SDR FDEA202106111500Frame · crackedDURING ROTO PROBE OF OPEN HOLES AT RH BS 1640 PER EO F-5310-E0344602. A CRACK INDICATION WAS NOTED IN THE BOTTOM INBD HOLE. THE CRACK IS IN THE FRAME AT APPROX. 3:00 O'CLOCK. COMPLIED WITH EA F-5310-T0361948 AND COMPLETED ALL STEPS 1-17 FUSELAGE - MAINFRSDR FDEA202106081470Pump · leakingPDIS 780 29-02 5505 08JUN21 IND OPEN U ON DESCENT HYDRAULIC SYSTEM PRESSURE ILLUMINATED. (L) RAN QRH, LEADING US TO USE ALTN GEAR EXTEND, LE, TE. SHGN 08JUN21 05:48 IND APON SHUSDR FDEA202106081469Floor Panel · delaminatedFLOOR PANEL 222AF IS DELAMINATED FLOOR BOARD 222AF FABRICATED ON TRAVELER # T21/1555539 IAW SRZ-25-005 MAJOR REPAIRSDR FDEA202106081467Floor Panel · delaminatedFLOOR PANEL 221AF IS DELAMINATED FLOORBOARD 221AF FABRICATED ON TRAVELER # T21/1555527 IAW DWG SRZ-25-005 MAJOR REPAIRSDR FDEA202105281417Circuit Card · faultedFWD CARGO DET 1 EICAS MESSAGE REPLACED AFOLTS CARD M10427 CARGO TESTS NORMAL REF M.M. 26-10-01-4.SDR FDEA202105251398Girt Bar · out of positionLEFT EVACUATION SLIDE LIGHT WILL NOT ARM REPOSITIONED GIRT BAR, ARMED DOOR AND SLIDE LIGHT ILLUMINATES, REF AMM 25-66-10-02. OK FOR SERVICESDR FDEA202105201332Frame · crackedLH FR 1640 S-14L LOWER INBD AND OUTBD HOLES HAVE CRACK INDICATIONS. INBD HOLE CLOCK POSITIONS AT 9 AND 3 O'CLOCK .OUTBD HOLE CLOCK POSITION AT 3 O'CLOCK. REFER TO EO F-5310-E0344602C PT1. COMPLIED WITH AND COMPLETED ALL STEPS 1-19 OF EA TF-5310-T0361285 PTSDR FDEA202105201331Frame · crackedRH FR 1640 S-14R LOWER INBD HOLE HAS A CRACK INDICATION. CLOCK POSITION BETWEEN 9 AND 6 O'CLOCK. REFER TO EO F-5310-E0344602C. COMPLIED WITH AND COMPLETED ALL STEPS 1-18 OF EA TF-5310-T0361295 PT1 FOR FRAME 1640 RH SIDE. TITLE: FUSELAGE - MAINFRAME - STA 1SDR FDEA202105141224Seat Track · damagedMCD SEAT TRACK AT STA. 579 LBL 45.50 LOBE IS BROKEN. INCOMING ACCOMPLISHED SEAT TRACK REPAIR AT LBL 45.50 BTW STA 570 & 640 IAW SRM 53-00-52-2R FIG 201. CAT A REPAIR MAJOR REPAIRSDR FDEA202105111171Floor Panel · delaminatedCOURIER FLOOR PANEL 221MBF DELAMINATED. FABRICATED FLOOR PANEL 221MBF ON VT MAE TRAVELER # T21/1549545 IAW DWG SRZ 25-0005 REV. R. CAT "A". MAJOR REPAIR.SDR FDEA202105111170Floor Panel · delaminatedCOURIER 222MAF FLOOR PANEL DELAMINATED. FABRICATED FLOOR PANEL 222MAF ON VTMAE TRAVELER # T21/1549543 IAW DWG SRZ25-005 REV R. CAT "A". MAJOR REPAIRSDR FDEA202105101166Floor Panel · delaminatedCOURIER FLOOR PANEL 222BF DELAMINATED FABRICATED COURIER PANEL 222 BF VT MAE TRAVELER # T21/1549546 IAW SRZ-25-0005 REV R CAT A MAJOR REPAIRSDR FDEA202105101165Floor Panel · delaminatedCOURIER 221AF FLOOR PANEL DELAMINATED FABRICATED COURIER FLOOR PANEL 221AF VT MAE TRAVELER # T21/1549544 IAW SRZ-25-0005 REV R CAT A MAJOR REPAIRSDR FDEA202105071156Bulkhead · dentedRH ECS BAY CUTOUT AFT BULKHEAD AT BODY STATION 1040 BULKHEAD FWD SIDE AS CHAFF MARKS LOCATED AT ECS BAY DOOR HOLD OPEN ROD FITTING AREA. CHAFFE/DENT FOUND TO BE OUT OF LIMITS IAW SRM 53-40-14-1A FIG 101. ACCOMPLISHED REPAIR IAW SRM 51-70-13-0G FIG 1. HFEC SDR FDEA202104220980Cusp Web · crackedMAIN CUSP AREA STA 640-660 LBL 62.5 AS VIEWED FROM BOTTOM FILLER PN BACF3F020B197NN CRACKED AT FASTENER LOCATION ACCOMPLISHED FEDEX EA # F-5321-T0361228-P1 FUSELAGE - CARGO COMP FLOORS - MAIN CABIN - STA 640 - LBL - 62.5 - CRACKEDSDR FDEA202104220973Seat Track · crackedMAIN CABIN - STA 580 SEAT TRACK IS CRACKED ACCOMPLISHED FEDEX EA # F-5310-T0361001-P1 : FUSELAGE - MAINFRAME - SEAT TRACK STA 580 LBL 45, CRACKED FLANGESDR FDEA202104210971Charger · no testL-1 DOOR OVERHEAD EXIT LIGHT DOES NOT ILLUMINATE DURING TEST. REPLACED EMERGENCY LIGHT BATTERY AND POWER SUPPLY ITEM M731 IAW AMM 33-51-07-2. OPS CHECKED EMERGENCY EXITS LIGHTS GOOD IAW AMM 33-51-01-2-0SDR FDEA202104200958Stub Frame · crackedMAIN CABIN FLOOR - STUB BEAM IS CRACKED REPAIRED STUB BEAM IAW FEDEX DWG SR57-53-004 AND EA: F-5310-T0361029: FUSELAGE - MAINFRAME - STA 580 FLOOR BEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR - REPAIR DOCUMENTATION AND REPETITIVE INSPECTIONS PER SR57SDR FDEA202104090861Proximity Sensor · contaminatedPASSING 13000 FT IN DESCENT TO KRST, RECEIVED EICAS ALERT L WING SLIDE . EMER DOORS LIGHT ALSO ILLUMINATED ON OVERHEAD PANEL. COMPLIED WITH QRH. NO OTHER UNUSUAL INDICATIONS. PERFORMED BITE TEST ON PROX BOX AND FOUND CODE 373 CONVERTS TO SENSOR S1037SDR FDEA202104080845Flap System · unknownAFTER TAKEOFF IN MODERATE TURBULENCE FLAPS 5 LIMIT SPEED (210 ITS)EXCEEDED. SPEED REACHED 213 ITS FOR 3 SECONDS WHILE FLAPS IN TRANSIT TO FLAPS 1. PERFORMED PHASE 1 INSPECTION REF B 757 AMM 05-51-08-2. NO DEFECTS NOTED A/C OK FOR SERVICE.SDR FDEA202103210737Guide Arm · out of adjustRAMP REPORTED L1 DOOR WOULD NOT OPEN FULLY. OPENS PARTIALLY AT THE TOP. BOTTOM STAYS ENGAGED. REMOVED FROM MEL STATUS. COMPLETED ADJUSTMENT OF L1 DOOR GUIDE ARM REF. B757 AMM 52-11-04-2, AND DOOR SDR FDEA202103200733Frame Splice · crackedDURING ACCOMPLISHMENT OF ROTO PROBE AT BS 1640 S-14L PER EO 5310-E0344602 PT1. THE BOTTOM OUTBD FASTENER HOLE HAD A CRACK INDICATION IN THE FRAME. WORK ACCOMPLISHED ON EA F-5310-T0359979 TITLE: FUSELAGE - MAINFRAME - STA 1640 FRAME SPLICE REPAIR BETWEEN ST
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