N923FD
Service difficulty reports · 142
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 = 'N923FD' 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 = 'N923FD' 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 FDEA202610201625Stringer · abnormalAFT CARGO BAY LOWER FRAME AT BS 1560, FOUND PREVIOUS REPAIR ON STR 26R.SDR FDEA202610201624Structure · corrodedNR 2 ENGINE PYLON STRUT, OTBD LOWER STRUCTURE NAC S 146.675 FOUND CORRODED.SDR FDEA202610191606Skin · corrodedNR 1ENGINE PYLON OUTB SIDE INTERNAL STRUCTURE SIDE SKIN CORRODED (PP STA 144.55 APROX.)SDR FDEA202610151595Strut · corrodedENG #2 PYLON STRUT INBD LOWER CHORD STA 144.425 CORROSION. THIS DISCREPANCY WAS ACCOMPLISHED ON EA # F-5430-T0389069 P1 TITLE: NACELLES / PYLONS-SKIN / PLATES / PANELS - CORROSION BLENDOUT #2 PYLON, LHS (INBD) SIDE SKIN DOUBLER INNER SURFACE, PP STA 153-16SDR FDEA202610121558Frame · corrodedRH ELEVATOR CONDUCTIVE FRAME MULTIPLE ZONES WITH CORROSION (UPPER AND LOWER) EVALUATED CONDUCTIVE FRAME RH ELEVATOR UPPER/LOWER HORIZONTAL STABILIZER AND REPLACED CONDUCTIVE SPLICE PLATE (02EA) AND SHIMS (02EA) UPPER/LOWER IAW B757 SRM 51-40-02-0G, SRM 55-SDR FDEA202610121557Frame · corrodedLEFT ELEVATOR CONDUCTIVE FRAME MULTIPLE ZONES WITH CORROSION (UPPER AND LOWER) EVALUATED CONDUCTIVE FRAME LH ELEVATOR UPPER/LOWER HORIZONTAL STABILIZER AND REPLACED CONDUCTIVE SPLICE PLATE (02EA) AND SHIMS (02EA) UPPER/LOWER IAW B757 SRM 51-40-02-0G, SRM 5SDR FDEA202610071490Seat Track · damagedMAIN CABIN SEAT TRACK BETWEEN BS 1080-1180, LBL 45.5. REMOVED AND REPLACED THE SEAT TRACK SECTION IAW SRM 51-40-02-OG, & DWG 144N5021, REV C.SDR FDEA202610071489Seat Track · corrodedMAIN CABIN SEAT TRACK BETWEEN STA 1140 TO STA 1160 RBL 45.50 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK SECTION ON MAIN CABIN FROM BS 1080 - 1180, RBL 45.5 IAW SRM 51-40-02-OG, & DWG 144N5021, REV C.SDR FDEA202610071488Seat Track · corrodedMAIN CABIN SEAT TRACK BETWEEN BS 1180 - 1200, RBL 45.50 WAS CORRODED. REMOVED AND REPLACED SEAT TRACK SECTION ON MAIN CABIN FROM BS 1180 - 1280, RBL 45.50 IAW SRM 51-40-02-OG, & DWG 146N5130 REV C.SDR FDEA202605220627Girt Bar · out of adjustLH ENTRY DOOR WILL NOT ARM. PERFORMED ADJUSTMENT OF L1 DOOR GIRT BAR. ARMED AND DISARMED L1 SLIDE MULTIPLE TIMES WITH GOOD INDICATION. DOOR ARMS AND DISARMS SMOOTHLY WITH NO BINDS. MEL CLEARED AND PLACARD REMOVED. A/C OK FOR SERVICE.SDR FDEA202604040400Bottle · emptyDURING MX PRE-FLIGHT, NOTICED THAT R1 DOOR EMERGENCY POWER RESEVOIR BOTTLE IS DEPLETED, READS 0 PSI. REMOVED AND REPLACED EMERGENCY POWER RESERVOIR FOR THE R1 DOOR W/REF TO B757 MM 52-11-30-4. ACFT OK TO CONTINUE.SDR FDEA202603020305Battery Pack · inoperativeEMERGENCY LIGHTS AT DOOR L1 INOPERATIVE. REPLACED DOOR L1 EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-07-2. OPS CHECKED GOOD.SDR FDEA202602110174Bulb · dimDURING MX PRE-FLIGHT FOUND R1 EMERGENCY EXIT SIGN DIM. REMOVED AND REPLACED 5 FAULTY BULBS AT THE R1 EMERGENCY EXIT SIGN IAW AMM 33-51-01-2 . OPS CHECK GOOD. ACFT OK FOR SERVICE.SDR FDEA202602110173Bulb · inoperativeDURING PRE-FLIGHT CHECK, FOUND CENTER OVERHEAD EMERGENCY EXIT IDENTIFIER SIGN DIM. AMM 33-51-01-2 FOUND CENTER OVERHEAD EMERGENCY EXIT SIGN HAS 14 FAULTY BULBS. REMOVED AND REPLACED 14 FAULTY BULBS AS PER ABOVE REF. OPS CHECK GOOD.SDR FDEA202602110172Bulb · inoperativeDURING PRE-FLIGHT FOUND L1 OVERHEAD EMERGENCY EXIT SIGN SLIGHTLY DIM. AMM 33-51-01-2 FOUND L1 OVERHEAD EMERGENCY EXIT SIGN HAS 5 FAULTY BULBS. REMOVED AND REPLACED 5 FAULTY BULBS AS PER ABOVE REF. OPS CHECKED GOOD.SDR FDEA202508281564Outflow Valve · failedDECLARED EMERGENCY DIVERTED TO IND. MECHS PERFORMED GVI OF PACK BAYS AND COMPONENTS. OUTFLOW VALVE CLEAR OF ANY DEBRIS, RAN LT PACK FOR LEAKS AND NO LEAKS DETECTED. WILL PROCEED WITH 757 AMM 21-51-00-5, PARG.10. SINGLE PACK PRESSURIZATION CONFIDENCE CHKSDR FDEA202508271550Controller · inoperativeAT FL350 RIGHT ENG BLEED EICAS FLICKERED THEN CABIN ALT HI DISCRETE LIGHT & EICAS ILLUM. CABIN RATE SHOWED A CLIMB OF 500-750 FT PER MIN & A CABIN ALT OF 12,000. DONNED O2 MASK. DESCENDED TO 10,000 FT. CABIN ALT INOP LIGHT ALSO ILLUM. DECLARED AN EMERGENCY. SDR FDEA202410281596Skin · crackedFREIGHT ULD HIT AIRCRAFT AND CREATED A HOLE ON R/H OF A/C AFT OF AFT CARGO DOOR UPDT 25OCT24 08:28 EWR SRM 53-00-00-0G DAMAGE FOUND AROUND STATION 1608 (SECTION 46) . DAMAGE DIMENSIONS ARE 10 FROM FWD TO AFT AND 9 FROM TOP TO BOTTOM WHILE BEING 2 1/SDR FDEA202304140648Lamp · burnedDURING SERVICE CHECK, FOUND R1 DOOR AND FLIGHT DECK DOOR OVERHEAD EMERGENCY LIGHTS SIGN (QTY:2) INOPERATIVE. RELEASED FOR SERVICE PER MEL : 33-51-01-01 CATEGORY : D EXPIRATION : 12AUG23 "MEL 33-51-01-01: INTERIOR EMERGENCY LIGHTS - INOP."MEL: 33-51-01-01SDR FDEA202301040198Seat Track · corrodedFOUND CRACK AND CORROSION ON SEAT TRACK BETWEEN STA 520 TO 560 AT LBL 45 ACCOMPLISHED REPAIR IAW FEDEX EA F-5310-T0372559 P1 TITLED : FUSELAGE- MAINFRAME-SEC 43, STA 520-560 AND LBL 45.5 SEAT TRACK UPPER FLANGE- CORROSION- REPAIR MAJOR REPAIRSDR FDEA202301040191Seat Track · corrodedFOUND CORROSION ON SEAT TRACK BETWEEN STA 350 TO 365 RBL 14 REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02 AND INSTALLED NRE FX 3504-3 SEAT TRACK IAW SRM 51-40-02 MAJOR REPAIRSDR FDEA202301040190Seat Track · corrodedFOUND CORROSION ON SEAT TRACK BETWEEN STA 350 TO 365 LBL 7 REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02 INSTALLED NEW FX3504-3 IAW SRM 51-40-02 MAJOR REPAIRSDR FDEA202301040188Seat Track · corrodedFOUND CORROSION ON SEAT TRACK BETWEEN STA 840 TO 860 AT RBL 45 REMOVED SEAT TRACK IAW SRM 51-40-02 ACCOMPLISHED REPAIR IAW SRM 53-00-52-2R, FIG. 201, REPAIR 1 MAJOR REPAIRSDR FDEA202301040187Not Entered · not enteredFOUND CORROSION ON INBD CREASE BEAM BETWEEN STA 860-880 LBL 64 REMOVED DAMAGED CREASE BEAM IAW SRM 51-40-02 ACCOMPLISHED REPAIR IAW FEDEX EA F-5310-T0372515 P1: FUSELAGE MAINFRAME: SEC 43, FLOOR STRUCTURE CREASE BEAM INNER CHORD, STA 860-880 LBL64. MAJOSDR FDEA202301040184Seat Track · corrodedFOUND CORROSION ON SEAT TRACK BETWEEN STA 560 TO 600 AT RBL 45 REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02 PERFORMED SETA TRACK REPAIR IAW SRM 53-00-52 REPAIR 1 MAJOR REPAIRSDR FDEA202301040182Crease Beam · corrodedFOUND CORROSION ON INBD CREASE BEAM BETWEEN STA 860 TO 880 AT RBL 64 ACCOMPLISHED REPAIR IAW FEDEX EA F-5310-T0372513 P1 FUSELAGE- MAINFRAME: SEC 43, FLOOR STRUCTURE, CREASE BEAM INNER CHORD, STA 860-880, RBL 64, PERMANENT REPAIR. MAJOR REPAIRSDR FDEA202301010199Splice · corrodedFOUND CORROSION ON AFT CARGO INNER SKIN SPLICE STRAP AT STA 1400 ADJACENT TO STRG 27L ACCOMPLISHED REPAIR IAW FEDEX EA F-5310-T0372415 P1 TITLED: FUSELAGE-MAINFRAME- STA 1400 BUTT SPLICE STRAP CORROSION REPAIR BETWEEN S-27L AND S-30 MAJOR REPAIRSDR FDEA202212290205Panel · crackedR/H WING SLAT #7 HAS A CRACK AFT EDGE NEAR ANTI ICE DOOR PERFORMED REPAIR FOR CLOSURE PANEL OF SLAT#7 PER SRM 57-43-01, REPAIR 10,PARAGRAPH 4.D, OPTION A. REF. SRM 57-43-01-1A,FIG. 101, NOTE "N". REP. DIM AND LOC.: 17" X 2". 12" FROM I/B AT L/E. REV. 138.1SDR FDEA202212290186Crease Beam · corrodedFOUND CORROSION ON INBD CREASE BEAM BETWEEN STA 1180 TO 1200 LBL 64 REMOVED AFFECTED PART IAW SRM 51-40-02 ACCOMPLISHED REPAIR IAW FEDEX EA F-5310-T0372399 P1 TITLED: FUSELAGE- MAINFRAME: SEC 46, FLOOR STRUCTURE , CREASE BEAM INNER CHORD , STA 1180-1200, LBSDR FDEA202212290185Floorbeam · corrodedFOUND CORROSION ON MAIN DECK FLOOR BEAM AT STA 1681 BETWEEN RBL 24 TO RBL 33 ACCOMPLISHED REPAIR IAW FEDEX EA F-5310-T0372416 P1 TITLED: FUSELAGE- GENERAL- STA 1681 RBL 22-27 CORROSION FOUND ON UPPER AFT AND FWD FLANGE. MAJOR REPAIRSDR FDEA202212290183Seat Track · corrodedFOUND CORROSION ON SEAT TRACK BETWEEN STA 1180 TO 1200 AT LBL 45 REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02 PART FAB. PER DWG 146N5130 AND FEDEX GMM 07-0-1001 SEE R/C W/O 20521483 INSTALLED SEAT TRACK IAW SRM 51-40-02 MAJOR REPAIRSDR FDEA2023012380154Floor Panel · wornDURING REMOVAL, FOUND FLOOR PANEL WORN. REPLACED THE FLOOR PANEL IAW DWG SRZ-25-005.SDR FDEA2023012380153Floor Panel · wornDURING REMOVAL FOUND FLOOR PANEL WORN. REPLACED THE FLOOR PANEL IAW DWG SRZ-25-005.SDR FDEA202212280147Floor Panel · wornDURING REMOVEL FOUND FLOOR P.N 11861182-15 WORN REPLACED MENTIONED FLOOR PANEL PER DWG SRZ-25-005. P/N: FX11861182-15 222MAF. MAJORSDR FDEA202212280146Floor Panel · wornDURING REMOVEL FOUND FLOOR PANEL P.N 11861182-16 WORN REPLACED MENTIONED FLOOR PANEL PER DWG SRZ-25-005 P/N: FX11861182-16 221MBF. MAJOR.SDR FDEA202212280145Floor Panel · wornDURING REMOVEL FOUND FLOOR PANEL P.N 141N5370-38 WORN REPLACED MENTIONED FLOOR PANEL PER DWG SRZ-25-005. P/N: FX141N5370-38. MAJOR.SDR FDEA202212280144Floor Panel · wornDURING REMOVEL FOUND FLOOR PANEL P.N 11861182-14 WORN REPLACED MENTIONED FLOOR PANEL PER DWG SRZ-25-005. P/N: FX11861182-14 222MBF. MAJOR.SDR FDEA202212280143Floor Panel · wornDURING REMOVEL FOUND FLOOR PANEL P.N 11861182-2 WORN REPLACED MENTIONED FLOOR PANEL PER DWG SRZ-25-005 P/N: FX11861182-2 222MDF. MAJOR.SDR FDEA202205241290Servo · malfunctionedPDIS 923 22-10 3694 24MAY22 BSL OPEN U WITH RIGHT AUTOPILOT ENGAGED THERE IS A CONSISTENT VIBRATION IN BOTH YOKES. THE LEFT AND CENTER AUTOPILOT DOES NOT HAVE THE VIBRATIONS. MEL 24MAY22 20:08 BSL U RELEASED FOR SERVICE PER MEL : 22-10SDR FDEA202205161236Holder · damagedMDIS 923 33-50 3670 16MAY22 HAJ FACT U RH EMERGENCY EXXIT LIGHTS DOES NOT ILLUMINATE R/I 16MAY22 19:09 HAJ U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 2013-1ASMI POS: 2 SRL: 3341 SDR FDEA202109302436Transmitter · faultedTE FLAP ASYM ON EXTENSION BETWEEN 0 AND 1 DEGREES. FOLLOWED QRH PROCEDURE AND DECLARED EMERGENCY. UNEVENTFUL LANDING. FIM 27-51 FAULT TREE 809 FOLLOWED: - FSEU #1 READOUT AT FLAPS 20 POSN RH 274.13 LH 253.59 - LT FLAP POSITION TRANSMITTER REQUIRES REPSDR FDEA202103160796Skin · dentedFOUND A DENT ON SLAT #6 O/B TRAILING EDGE 10.5" FROM O/B TO 3.8" FROM TOP REPAIRED #6 SLAT UPPER T/E WEDGE 9.752 FROM OUTBOARD EDGE AND 4.5" FROM UPPER IAW IAW SRM 57-43-02-2R REPAIR 4 FIG 201 THIS IA A CAT A MAJOR REPAIRSDR FDEA202103030546Flap Track · looseR/H O/B MAIN FLAP TRACKS #7 AND #8 ARE LOOSE AT AFT ATTACH POINTS REPLACED AFT ATTACH POINTS HARDWARE ON R/H O/B MAIN FLAP TRACKS #7 AND #8 IAW AMM 27-51-15SDR FDEA202103030544Flap Track · looseL/H O/B MAIN FLAP TRACKS #1 AND #2 ARE LOOSE AT AFT ATTACH POINTS. REPLACED AFT ATTACH POINTS HARDWARE ON L/H O/B MAIN FLAP TRACKS #1 AND #2 IAW AMM 27-51-15SDR FDEA202102190761Drag Fitting · corrodedCORROSION FOUND DURING NOT INSPECTION ON L/H ENG #1 DRAG AND DIALONAL BRACE IN THE FOLLOWING HOLES 2,3,6,8,9,10,14,16 REMOVED CORROSION FROM HOLES #2,3,6,8,9,10,14,16, AND 16. CRACKS FOUND AT HOLES #3 AND #9. REPLACED INBOARD AND OUTBOARD DRAG BRACE FITTING ISDR FDEA202102180762Drag Fitting · corrodedCORROSION FOUND DURING NDT INSPECTION ON RH ENG #2 DRAG FITTING DIAGONAL BRACE HOLES #1, 2, 3, 5, 6, 8, 10, 11, 13, 14, 15, 16, 17, AND 18. REMOVED CORROSION FROM HOLES #1, 2, 3, 5, 6, 8, 10, 11, 13, 14, 15, 16, 17, AND 18. CRACKS FOUND AT HOLES #4 AND #9. REPSDR FDEA202102160446Fill Port · corrodedR/H OVERWING FILL PORT FAILED BONDING CHECK. HAVE EVIDENCE OF CORROSION EVALUATED R/H OVERWING FILL POART IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 3, FIG 102 AND FOUND FILL PORT TO BE OUTSIDE SRM LIMITS.LIMIT OF REMAINING THICKNESS 0.240" ACTUAL=0.210". REPAIREDSDR FDEA202102160445Fill Port · corrodedL/H OVERWING FILL PORT FAILED BONDING CHECK HAS EVIDENCE OF CORROSION EVALUATED L/H OVERWING FILL POART IAW SRM 57-20-01-1A ALLOWABLE DAMAGE 3, FIG 102 AND FOUND FILL PORT TO BE OUTSIDE SRM LIMITS. LIMIT OF REMAINING THICKNESS 0.240" ACTUAL=0.220". REPAIRED SDR FDEA202009142211Switch · out of adjustPDIS 923 52-70 1907 14SEP20 CDG OPEN U. MN CARGO DR SYS ON STATUS PAGE AFTER BLK OUT FROM BSL INFO 14SEP20 18:20. MC1 R REF TECH TIP NR 18-0045 FACT 15SEP20 09:35 CDG, AS PER FIM 52-72-00-815-802 CLEANNING CONNECTORS D7174 OF S10518 AND D7170 OF V10129. PERSDR FDEA202009032085Hose · leakingPDIS 923, 32-51, 1866, 03SEP20, AMS, OPEN U. AT APPROX 500' ON LANDING, RECEIVED 'L HYD QTY' EICAS. OBSERVED QTY SLOWLY DECREASING. AFTER LANDING RECEIVED 'L HYD SYSTEM PRESSURE' EICAS, QTY=0.16 SHGN 03SEP20 09:25. AMS U DURING T/S FOUND FLEX HYDR. H
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