N920FD
Service difficulty reports · 222
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N920FD' AND registry_match = 'registration' 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 n_number = 'N920FD' AND registry_match = 'registration' 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 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 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 FDEA202311211876Floor Panel · dentedFOUND 2EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11862182-13 BTW RBL 46-50 AND STA 720- 780. REMOVED FLOOR PANEL P\N 11864182-13 FROM STA 720-780 IAW B-757 AMM 53-01-01-4, EVALVATED AND REPAIRED 2 EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1 DETSDR FDEA202311211875Floor Panel · dentedFOUND 3EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11862182-21 BTW RBL 46-50 AND STA 780- 880. REMOVED FLOOR PANEL #11862182-21 FROM STA 780 - 880 IAW (B 757) AMM 53-01-01-4, EVALUATED AND REPAIRED 3EZ DENTS ON FLOOR PANEL IAW B757 SRM 53-00-50-R2 REP 1 DETAIL SDR FDEA202311211874Floor Panel · dentedFOUND 2EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11864182-10 BTW RBL 46-50 AND STA 1320- 1420. REMOVED FLOOR PANEL P\N 11862182-10 FROM STA 1320-1420 BTW RBL 46-50 IAW B-757 AMM 53- 01-01-4, EVALUATED AND REPAIRED 2EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-5SDR FDEA202311211873Floor Panel · dentedFOUND 3EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-2 BTW RBL 46-50 AND STA 900- 1020. REMOVED FLOOR PANEL P\N 11862182-2 FROM STA 900-1020 BTW IAW B-757 AMM 53-01-01-4, EVALUATED AND REPAIRED 3EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1 SDR FDEA202311211872Floor Panel · dentedFOUND DENT AT MAIN CARGO FLOOR PANE; P\N: 11862182-28 BTW RBL 46-50 AND STA 880-900 REMOVED FLOOR PANEL P\N 11862182-28 FROM STA 880-900 BTW RBL 46- RBL 50 IAW B-757 AMM 53-01-01-4, EVALUATED AND REPAIRED 1EA DENT ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R RSDR FDEA202311211871Floor Panel · dentedFOUND 6EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11864182-2 BTW RBL 46-50 AND STA 1200- 1320. REMOVED FLOOR PANEL P\N 11864182-2 FROM STA 1200-1320 IAW B-757 AMM 53-01-01-4, EVALVATED AND REPAIRED 6 EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1 DESDR FDEA202311211870Floor Panel · dentedFOUND 4EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-26 BTW RBL 46-50 AND STA 1100- 1200. REMOVED FLOOR PANEL P\N 11863182-26 FROM STA 1100-1200 IAW B-757 AMM 53-01-01-4, EVALVATED AND REPAIRED 4EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-R2 REP 1 DETSDR FDEA202311211869Floor Panel · dentedFOUND 3EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-38 BTW RBL 46-50 AND STA 1055- 1100. REMOVED FLOOR PANEL P\N 11862182-38 FROM STA 1055-1100 IAW B-757 AMM 53-01-01-4, EVALUATED AND REPAIRED 3EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1 DSDR FDEA202311211868Floor Panel · dentedFOUND 2EA DENTS AT MAIN CARGO FLOOR PANEL P\N: 11863182-34 BTW RBL 46-50 AND STA 1020- 1055. REMOVED FLOOR PANEL P\N 11862182-34 FROM STA 1020-1055 IAW B-757 AMM 53-01-01-4, EVALUATED AND REPAIRED 2EA DENTS ON FLOOR PANEL IAW B-757 SRM 53-00-50-2R REP 1 SDR FDEA202311201865Floorbeam · corrodedMAIN CABIN FLOOR BEAM AT STA 880 LBL 48 TO 62 LBL SURFCE CORROSION. DOT 101. ACCOMPLISHED EA F-5321-T0376857 P1 "FUSELAGE MAINFRAME SECTION 43, FLOOR BEAM ASSY CORROSION, STA879, UPPER CHORD, LBL 45-58, DEVIATION FROM TYPICAL SRM REPAIR, WITH NO DEVIATION.SDR FDEA202311191864Frame · unknownDURING FUSELAGE MAINFRAME - AFT CARGO COMPARTMENT FRAME INSPECTION PER EO NO. F- 5310-E0347443 B P1 EXISTING REPAIR WAS FOUND AT STA 1300 BTW STRG 26L-27L CONTACT SERVICE ENGINEERING FOR ALTERNATIVE INSPECTION. ACCOMPLISHED EA NO. T F-5310-T0376726 P1. FUSSDR FDEA202311061834Slat · debonded#5 SLAT FOUND DISBONDED. INSTALLATION OF #5 SLAT TO BE ACCOMPLISHED ON NR00110. NR ATTACHED. REPAIRED DISBONDING ON #5 SLAT IAW B757 SRM 51-70-10-2R, B757 SRM 51-20-01-0G, AND B757 AMM 51-21-15-7.SDR FDEA202311061833Slat · debonded#2 SLAT FOUND DISBONDED. REMOVED AND REINSTALLED #2 SLAT FOR DISBONDING REPAIR IAW B757 AMM 27-81-02-4, B757 SRM 51-70-10-2R, B757 SRM 51-20-01-0G, B757 AMM 51-21-15-7. OPS CHECK GOOD IAW B757 AMM 27-81-02-4. REPAIRED #2 SLAT IAW SRM (B757) 57-43-02-2R.SDR FDEA202311061832Skin · debonded#8 SLAT FOUND DISBONDED. REMOVED AND REINSTALLED #8 SLAT FOR DISBONDING REPAIR IAW B757 SRM 51-70-10-2R, B757 AMM 27-81-02-4, B757 AMM 51-21-15-7, AND B757 SRM 51-20-01-0G. OPS CHECK GOOD IAW B757 AMM 27-81-02-4. REPAIRED #8 SLAT IAW SRM (B757) 57-43-02-2RSDR FDEA202309261652Unknown · unknownPDIS 920 32-51 5203 26SEP23 TLV FACT U AFTER LANDING NOSEWHEEL MADE A CLUNKING SOUND WHEN ENGAGING TILLER TO TURN. I.A.W FIM 32-51 FAULT TREE 813 BLOCK 1, STEERING MEETERING VLV COVER REMOVED, AREA INSPECTED FOUND OK. I.A.W BLOCK 2 FOUND MISSISDR FDEA202302220331None · nonePDIS 920 25-60 4604 22FEB23 CDG FACT U SLIDE LIGHT DOES NOT ILLUMINATE WHEN MAIN ENTRY DOOR CLOSED AND ARMED. FACT 22FEB23 02:16 CDG U AMM 25-66-01-6 PERFORMED OPS CHECK OF LEFT PASSENGER DOOR SLIDE SYSTEM AS PER AMM 25-66-01-6. OPS CHECKSDR FDEA202301190139Bulb · failedPDIS 920 52-10 4503 19JAN23 CDG FACT U DOOR L1 SLIDE LIGHT BURNT OUT FACT 19JAN23 18:59 CDG U AMM: 52-11-25-5 REBULBED SLIDE LIGHT AS PER SWPM AND TESTED OK IAW AMM 52-11-25-5. A/C OK FOR SERVICE.SDR FDEA202301110068Bulb · failedPDIS 920 33-50 4480 11JAN23 BER FACT U SLIDE ARMED LIGHT ON L1 OUT FACT 11JAN23 11:26 BER U AMM: 33-51-06-2-1 REV.130.13 BULB,S REPLACED ON SLIDE LIGHT ARMED / DISARMED INDICATOR , SLIDE ARMED / DISARMED FUNCTION CHECKED , O.K. , ACC.AMM 33SDR 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 FDEA202205121193Transmitter · faultedPDIS 920 27-50 3732 12MAY22 CDG OPEN U TE FLAP DISAGREE WHEN SELECTING FLAP 20. RAN QRH, USED ALTN FLAP CONTROLLER TO LAND FLAPS 20. ***EMERGENCY DECLARED*** SHGN 13MAY22 00:26 CDG U CHECKED FAULTS IN FSEU 1 FOUND FLAP DISAGREE AND LEVSDR FDEA202203090595Adc · unknownPDIS 920 34-16 3550 19MAR22 CDG OPEN U ON CLIMB THRU APPROXIMATELY FL280, THE FIRST OFFICER S SPEED TAPE READ, NO SPD AND THE ALTIMETER JUMPED SEVERAL HUNDRED FEET FOR APPROXIMATELY 1 SECOND BEFORE RETURNING TO NORMAL. RH AND LH AIR DATA COMSDR FDEA202201190099Floor Panel · wornMAIN DECK FLOOR PANEL #223MDF STATION 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRZ-25-005 REF. ENGINEERING DISPOSITION OF RFTA NO:02841-0205. MAJOR REPAIRSDR FDEA202201190098Floor Panel · wornMAIN DECK FLOOR PANEL #221BF STA 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRX-25-005 REF. ENGINEERING DESPOSITION OF RFTA NO:02841-0205. MAJOR REPAIRSDR FDEA202201190096Floor Panel · wornMAIN DECK FLOOR PANEL #222 MAF STA 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRZ 25-005 REF. ENGEENIRING DISPOSITION OF RFTA NO: 02841-0205. MAJOR REPAIRSDR FDEA202201160075Floor Panel · wornMAIN DECK FLOOR PANEL #221MBF STA 297 TO 440 FOUND WORN FABRICATED MENTIONED PANEL PER FEDEX SRZ-25-005. REF ENGINEERING DISPOSITION OF RFTA NO: 02841-0205. MAJOR REPAIRSDR 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 FDEA202112280178Seat Track · corrodedFOUND CORROSION ON SEAT TRACK BL 0, STA 1330-1320. WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA # F-5310-T0366212SDR FDEA202112280168None · corrodedFOUND CORROSION ON FLOOR BEAM EXISTING REPAIR AT STA 1320 BETWEEN RBL24 TO RBL45 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX EO # F-5310-T0366466SDR FDEA202112280167Seat Track · corrodedFOUND CORROSION ON SEAT TRACK RBL 45 BETWEEN STA 1320 TO 1420 PERFORMED SEAT TRACK REPAIR USING NEW FABRICATED 2 EA SEAT TRACKS SECTION, 2 EA SPLICES , AND 1 EA STRAP PER SRM 53-00-52, REPAIR 1 FIG. 201, THIS REPAIR IS A PERMANENT CAT. A REPAIR, THE INSP. SDR FDEA202112280166Seat Track · corrodedFOUND CORROSION ON SEAT TRACK RBL 24 ON STA 1320 AND STA 1410 PERFORMED SEAT TRACK REPAIR USING NEW FABRICATED SEAT TRACK SECTION, 2 EA SPLICES , AND 1 EA STRAP PER SRM 53-00-52 REPAIR 1 , FIG 201, THIS REPAIR IS A PERMANENT CAT "A" REPAIR , THE INSP. GISDR FDEA202112280122Frame · unknownFOUND UNDOCUMENTED WEB REPAIR AT STA 1375 OUTBD CREASE BEAM ON R/H SIDE PERFORMED DVI PER SRM 51-10-08. REPAIR EVALUATED I.A.W BOEING SR:1-198375510 AND NO DAMAGE OR DEVIATIONS NOTED. THIS IS A MAJOR REPAIRSDR FDEA202112090121Frame Splice · unknownEVALUATE SUPPORT AT STA 1020, STR 5L & 5R PER EO 5100-7-5001 PERFORMED DVI PER SRM 51-10-08. REPAIR EVALUATED I.A.W EA F-5310-T0366310 AND NO DAMAGE OR DEVIATIONS NOTED. THIS IS A MAJOR REPAIR.SDR FDEA202112090120Frame Splice · unknownEVALUATE SUPPORT AT STA 980, S-5L PER EO 5100-7-5001 PERFORMED DVI PER SRM 51-10-08 REPAIR EVALUATED I.A.W EA F-5310-T0366306 AND NO DAMAGE OR DEVIATIONS NOTED. THIS IS A MAJOR REPAIRSDR FDEA202112090119Frame Splice · unknownEVALUATE SUPPORT AT STA 1100, S5L TO S-5R PER EO 5100-7-5001 PERFORMED DVI PER SRM 51-10-08 REPAIR EVALUATED I.A.W EA F-5310-T0366309 AND NO DAMAGE OR DEVIATIONS NOTED. THIS IS A MAJOR REPAIRSDR FDEA202111222930None · damagedPDIS 920 25-10 3302 22NOV21 CDG FACT U FO SHOULDER RESTRAINTS DO NOT RETRACT. FACT 23NOV21 11:54 CDG INSPECTED F/O SEAT SHOULDER HARNESS PER MM 25-11-00-17 OPS CHECK OK THE REASON WHY THE SHOULDER HARNESS DOESN'T RETRACT TO THE SAME SDR FDEA202108262099Line · unsecureL1 DOOR DIFFICULT TO CLOSE AND ARM FOUND EMERGENCY SLIDE STATIC LINE LOOSE AND BUCKLE DANGLING CAUSING INTERFERENCE. REPOSITIONED IAW AMM 25-66-01-4. OPS TEST OKAY.SDR 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 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 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 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.SDR FDEA2020061981284Girt Bar · out of adjustR1 DOOR IS VERY STICKY TO DISARM. PERFORMED RT DOOR GIRT BAR ADJUSTMENT PER AMM 52-11-25-5-0. PERFORMED OPERATIONAL CHECK ON RT DOOR AND FOUND OK PER THE SAME AMM 52-11-25-5-0.SDR FDEA2020061091158Unknown · malfunctionedUNABLE TO ARM RIGHT FWD ENTRY DOOR. OPS CHECK PER AMM 52-11-00-5, TEST SATIS, A/C OK FOR SERVICE.SDR FDEA2020051390843Slide · unserviceableL1 DOOR ESCAPE SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED LH ENTRY DOOR SLIDE PER B757 MM25-66-01-4. OPS CHECK GOOD AIRCRAFT GOOD FOR SERVICE PART NUMBER D30654-122. SERNP M8047 MANUFACTER AIR CRUSERS SLIDE RAFTSDR FDEA2020043090843Slide · out of limitsL1 DOOR ESCAPE SLIDE PRESSURE OUT OF LIMITS. REMOVED AND REPLACED LH ENTRY DOOR SLIDE PER B757 MM25-66-01-4. OPS CHECK GOOD AIRCRAFT GOOD FOR SERVICE PART NUMBER D30654-122. SERNP M8047 MANUFACTER AIR CRUSERS SLIDE RAFTSDR FDEA2020021490329Skin · damagedMDIS 920 51-00 1440 09FEB20 LGG OPEN U AFT CARGODOOR AND SKIN BEHIND GOT HIT BY ULD ON THE DRIFT WITH HIGH WINDS, CARGO DOOR HAS A HOLE , SKIN BEHIND IS DEFORMED, DAMAGED TO BE ASSESSED, AIRCRAFT DOWN. COMPLIED WITH E A F-5330-T0352406 PT1 SDR FDEA201912133242Floor Panel · damagedAFT CARGO PANEL # 161AF DAMAGED REPLACED AFT CARGO PANEL 161AF IAW FEDEX GMM 7-0-1001 AND BOEING DRAWING # 453N1805.
Back to N920FD