N923FD
Service difficulty reports · 143
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 FDEA201201240324Seat Track · corrodedSHEAR PLATE SEAT TRACK SPLICES AT LBL 24.75 FOUND CORRODED FROM BS 418 TO 440. SHEAR PLATE SEAT TRACK SPLICES REPLACED IAW DWG 3458 AND SRM 51-40-02.SDR FDEA201201240323Seat Track · corrodedLT OTBD MAIN DECK SEAT TRACK FOUND CORRODED AT STN 1034 SEAT TRACK, REPAIRED IAW EA F-5340157285.SDR FDEA201201240322Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND CORRODED AT AREA UNDER BS 980. LT STUB BEAM CENTER TANK UPPER SKIN REPAIRED IAW EA F-5710-157292 & F-5710-157283.SDR FDEA201201240321Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND CORRODED AT AREA UNDER BS 1000 LT STUB BEAM. CENTER TANK UPPER SKIN REPAIRED IAW EA F-5710-157286 & F-5710-157286.SDR FDEA201201240320Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND LIGHT SURFACE CORROSION AT AREA UNDER BS.960. RT STUB BEAM CENTER TANK UPPER SKIN REPAIRED IAW EA F-5710-157284.SDR FDEA201201230314Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND LIGHT CORROSION AT AREA UNDER BS.1020 RT STUB BEAM CORROSION. REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT. CARRIED OUT IAW SRM 57-10-01 FOUND WITHIN LIMITS.SDR FDEA201201230313Panel · corrodedCENTER TANK UPPER SKIN FOUND LIGHT SURFACE CORROSION AT AREA UNDER BS.920 LT STUB BEAM CORROSION. REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT CARRIED OUT IAW SRM 57-10-01 FOUND WITHIN LIMITS.SDR FDEA201201230312Panel · corrodedCENTER TANK UPPER SKIN FOUND LIGHT SURFACE CORROSION AT AREA UNDER BS 920 RT STUB BEAM CORROSION REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT CARRIED OUT IAW SRM 57-10-01. FOUND WITHIN LIMITS.SDR FDEA201201230311Panel · corrodedCENTER TANK UPPER SKIN FOUND LIGHT SURFACE CORROSION AT AREA UNDER BS.940 RT STUB BEAM CORROSION REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT. CARRIED OUT IAW SRM 57-10-01 FOUND WITHIN LIMITS.SDR FDEA201201230310Fuel Cell · corrodedCENTER TANK UPPER SKIN FOUND CORRODED AT AREA UNDER BS.940 LT STUB BEAM CORROSION. REMOVED AND REPROTECTED IAW SRM 57-10-01 AND DAMAGE ASSESSMENT CARRIED OUT IAW SRM 57-10-01, FOUND WITHIN LIMITS.SDR FDEA201201230306Strut · corrodedLEFT ENGINE, CNA SIDE STRUT AT 9 O'CLOCK AFT LOOKING FORWARD UPPER SURFACE CORRODED. SIDE STRUT REPLACED.SDR FDEA201201180243Crease Beam · corrodedCREASE BEAM WEB BETWEEN STA 1300-1320 RT CORRODED CREASE BEAM WEB REPLACED IAW DWG 146N8322 AND SRM 51-40-02.SDR FDEA201201180241Thrust Reverser · corrodedCORROSION FOUND ON TRANSLATING SLEEVE OUT SKIN. THRUST REVERSER ASSEMBLY REPLACED.SDR FDEA201008103007Lamp · inoperativeSLIDE LIGHT WILL NOT ILLUMINATE WHEN DOOR IS ARMED. RELAMPED SLIDE LIGHT IAW SMP OPS CHECKS NORMAL. RELAMPED SLIDE LIGHT IAW SMP OPS CHECKS NORMAL. FINAL CLOSEDSDR FDEA201007032340Computer · malfunctionedON TAKEOFF PASSING 9,000 FT T/E FLAP DISAGREE EICAS ANNUNCIATED INTERMITTENTLY. ATB BACK TO KFSD, RAN T/E FLAP DISAGREE CHECKLIST, LANDED WITHOUT INCIDENT. T/E FLAP DISAGREE EICAS MSG WAS INTERMITTENT ON AND OFF THROUGH OUT THE FLIGHT. R AND R LT EICAS COMSDR FDEA201007032339Flap System · malfunctionedON TAKEOFF PASSING 9,000 FT T/E FLAP DISAGREE EICAS ANNUNCIATED INTERMITTENTLY. ATB BACK TO KFSD, RAN T/E FLAP DISAGREE CHECKLIST, LANDED WITHOUT INCIDENT. T/E FLAP DISAGREE EICAS MSG WAS INTERMITTENT ON AND OFF THROUGH OUT THE FLIGHT.SDR FDEA200903080866Floor Support · corrodedCORROSION ON FLOOR SUPPORT CHANNEL LOCATED AT RBL 60, WL 208 AT STATION 1661 TO STATION 1681. EVALUATE AND RECTIFY. CHANNEL WAS REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-40-02 REVISION 95. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR FDEA200903080862Gate · corrodedCORROSION ON BOTTOM DOOR GATE OF NUMBER ONE LEFT PASSENGER DOOR. EVALUATE AND RECTIFY. L1 DOOR BOTTOM GATE WAS REMOVED AND REPLACED IN ACCORDANCE WITH B757-200 AMM CHAPTER 52-11-38 REVISION 56. REPAIR IS CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100 CRITERIASDR FDEA200903060859Web · corrodedSHEAR WEB FOUND CORRODED LOCATED AT BS 600 TO BS 620 RIGHT. EVALUATE AND REPAIR. SHEAR WEB AT BS 600 TO BS 620 WAS REMOVED AND REPLACED IN ACCORDANCE WITH SRM 51-40-02 REVISION 96 AND DRAWING 143N5520-10. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERSDR FDEA200903040838Skin · corrodedTWENTY AREAS WITH CORROSION ON NUMBER TWO CARGO DOOR INTERNAL SKIN SURFACE. EVALUATE AND RECTIFY. MINOR SURFACE CORROSIONS ON NUMBER TWO CARGO DOOR INTERNAL SKIN SURFACE WERE BLENDED OUT IN ACCORDANCE WITH SRM 51-10-02 REVISION 95. AREA EVALUATED AND FOUND SDR FDEA200903040837Skin · corrodedCORROSION IN BETWEEN FRAME OF INTERIOR SURFACE LOWER CENTER SECTION OF AUXILIARY POWER UNIT ACCESS PANEL 315AL. EVALUATE AND REPAIR. REMOVED AND REPLACED SKIN OF AUXILIARY POWER UNIT ACCESS PANEL 315AL IN ACCORDANCE WITH FEDEX EA F-5240-124398, TITLE: DOORSDR FDEA200903040836Skin · corrodedWIDESPREAD PITTING CORROSION ON THE RIGHT EXTERNAL SKIN OF AUXILIARY POWER UNIT ACCESS DOOR. EVALUATE AND RECTIFY. RIGHT AUXILIARY POWER UNIT ACCESS DOOR SKIN WAS REMOVED AND REPLACED IN ACCORDANCE WITH EA F5240-126205, REPAIR CLASSIFIED AS MINOR AS PER SDR FDEA200903020787Gate · corrodedCORROSION LOCATED AT CORNER ON CABIN LEFT NUMBER FOUR PASSENGER DOOR TOP DOOR GATE. EVALUATE AND RECTIFY. LEFT NUMBER FOUR DOOR TOP DOOR GATE WAS REMOVED AND REPLACED IN ACCORDANCE WITH B757-200 AMM CHAPTER 52-11-38 REVISION 56. REPAIR CLASSIFIED AS MINORSDR FDEA200903020786Channel · corrodedSURFACE CORROSION FOUND ON LT UNDER WING FAIRING197DL SUPPORT STRUCTURE LOWER CHANNEL LOCATED AT BS 1090 TO BS 1094 AREA. EVALUATE AND RECTIFY. SUPPORT STRUCTURE LOWER CHANNEL LOCATED AT BS 1090 TO BS 1094 WAS REMOVED AND REPLACED IN ACCORDANCE WITH EA F-533SDR FDEA200902260726Web · crackedWEB INTERCOSTAL AT STATION 1320, RBL 45.0, WATER LINE 206.0 FOUND WITH 2.0 INCH CRACK REPAIR. REMOVED AND REPLACED CRACKED SHEAR WEB IAW SRM 51-40-02, REV 95. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.SDR FDEA200902240682Floor Support · corrodedFWD CARGO COMPARTMENT FLOORBEAM BS 640 TO 680, RBL 2.9 HAS CORROSION AROUND THREE ANCHOR NUT HOLES. CORROSION FOUND EXCEEDED B757 SRM 53-00-53 REV 95 DAMAGE LIMITS. CHANNEL REPLACED IAW B757 SRM 51-70-11 REV 95. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100SDR FDEA200902230672Crease Beam · corrodedCORROSION FOUND ON CREASE BEAM WEB RUNNING INTO FLOORBEAM LOCATED AT AFT CARGO COMPARTMENT BETWEEN STA 1360 AND STA 1380 RIGHT SIDE. REPAIR AS REQUIRED. REPLACED CREASE BEAM WEB IAW SRM 53-60-13 FOR REMOVAL AND SRM 51-40-02 FOR INSTALLATION. THE CREASE BEAMSDR FDEA200902210622Gate · corrodedRT NR 4 PAX DOOR LOWER GATE HAS INTERGRANULAR CORROSION. RT NR 4 PAX DOOR LOWER GATE CORROSION FOUND EXCEEDED ALLOWABLE DAMAGE LIMITS IN SRM 52-10-02 REV 95. LOWER GATE REPLACED IAW AMM 52-11-38. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR FDEA200902210621Gate · corrodedRT NR 4 PAX DOOR UPPER CORNER (INTERNAL) HAS CORROSION. RT NR 4 DOOR UPPER GATE CORROSION FOUND BEYOND ALLOWABLE DAMAGE LIMITS IN SRM 52-10-02 REV 95. DOOR TOP GATE REPLACED IAW AMM 52-11-38 REV 56. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR FDEA200902210620Gate · corrodedCABIN, L2 DOOR TOP GATE HAS INTERGRANULAR CORROSION. CORROSION ON L2 DOOR TOP GATE FOUND EXCEEDED LIMITS IN SRM 52-10-02 REV 95. DOOR TOP GATE REPLACED IAW AMM 52-11-38. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR FDEA200902200617Gate · corrodedNR 2 LEFT PAX DOOR BOTTOM GATE HAS CORROSION. L2 DOOR BOTTOM GATE CORROSION FOUND EXCEEDED ALLOWABLE DAMAGE LIMITS IN B757 SRM 52-10-02 REV 95. GATE REPLACED IAW B757 AMM 52-11-38 REV 56. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR FDEA200902200616Gate · corrodedCABIN NR 2 RIGHT DOOR LOWER DOOR GATE HAS CORROSION AT CORNER (INTERNAL) R2 DOOR BOTTOM GATE CORROSION FOUND EXCEEDED ALLOWABLE LIMITS IN B757-200 SRM 52-10-02. DOOR GATE REPLACED IAW B757-200 AMM 52-11-38 REV 56. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-10SDR FDEA200902160557Frame · corrodedLOWER FUSELAGE AFT WING TO BODY FAIRING UPPER FRAME NUTPLATE STRIP HAS INTERGRANULAR CORROSION BETWEEN STA 1220 AND STA 1240, LBL 63.0, AFT OF NUMBER 1 ELECTRIC MOTOR PUMP OF CENTER HYDRAULIC SYSTEM. EVALUATE AND RECTIFY. CORRODED LOWER CHORD REMOVED AND RSDR FDEA200902160556Angle · corrodedAFT CARGO COMPARTMENT BETWEEN STA 1360 AND 1365 HAS EXFOLIATION CORROSION ON SUPPORT ANGLE FOR CREASE BEAM WEB WATER LINE 207.5 RIGHT SIDE TUNNEL SUPPORT ANGLE REMOVED AND REPLACED BY FABRICATION PER BOEING DRAWING 146N8326 USING 7075 - T0 0.040 THICK. REPAISDR FDEA200902160555Stringer · corrodedCORROSION ON STRINGER L16 LOCATED AT CABIN STA 1360 AND STA 1380. EVALUATE AND RECTIFY. SPLICE REPAIR CARRIED OUT ON STRINGER L16 BETWEEN STA 1360 AND STA 1380 IN ACCORDANCE WITH SRM 53-00-03 REV 95 FIGURE 201, REPAIR 1, DETAIL 11. REPAIR CLASSIFIED AS MAJSDR FDEA200902160554Floorbeam · corrodedCORRODED FLOOR SUPPORT AT RBL 3, 11, AND 16 LOCATED AFT CARGO AT BS 1200 TO BS 1380. EVALUATE AND REPAIR, AT BS 1200 TO BS 1380 FLOOR SUPPORTS AT RBL 3 AND RBL 6 CORROSION BLENDED OUT AND FOUND WITHIN ALLOWABLE LIMIT IN ACCORDANCE WITH B757-200 SRM 53-00-53, SDR FDEA200902090483Frame · corrodedFORWARD ACCESSORY COMPARTMENT FRAME AT BS 231.25 BETWEEN S29L TO 29R HAS SEVERAL GOUGES. REPAIR CARRIED OUT AS PER EA F-5310-111009 A, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 CRITERIA.SDR FDEA200902010409Support Frame · corrodedLOWER FUSELAGE, SUPPORT FRAME HAS INTERGRANNULAR CORROSION AT STA 1180, RBL 7.0 TO 29.0 AT KEELBEAM. REPLACED IAW DWG 149N7528 AND SRM 51-40-02. REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 CRITERIA.SDR FDEA200901060048Floor Support · corrodedFWD CARGO COMPARTMENT FLOOR SUPPORT FROM BS 640 TO BS 680, LBL 2.9 FOUND WITH CORROSION AROUND EIGHT ANCHOR NUT HOLES. CORROSION ON STRINGER FROM BS 640 TO BS 680 FOUND EXCEEDED ALLOWABLE LIMITS IAW SRM 53-00-53 REV 95. FLOOR SUPPORT REPLACED IAW B757-200 SDR FDEA200812035059Floorbeam · corrodedEXISTING REPAIR WAS FOUND ON CABIN FLOORBEAM UPPER CHORD AT BS 365.25 BETWEEN RBL 18 AND RBL 54. TO EVALUATE AND REPAIR AS REQUIRED. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT1 AND FOUND REPAIR WAS PREVIOUSLY ACCOMPLISHED LIMITED REPAIR NR RS/75SDR FDEA200812035058Crease Beam · corrodedEXISTING DOUBLER REPAIR WAS FOUND ON LT CREASE BEAM WEB BETWEEN BS 1060, LBL 70. TO EVALUATE AND REPAIR AS REQUIRED. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT1 AND FOUND PREVIOUSLY ACCOMPLISHED BY BRITANNIA AIRWAYS LIMITED REPAIR NR RS/757/53/732 SDR FDEA200812035057Crease Beam · corrodedEXISTING REPAIR WAS FOUND ON RT CREASE BEAM INBOARD CHORD AT BS 660. TO EVALUATE AND REPAIR AS REQUIRED. EXISTING REPAIR EVALUATED AS PER EO F-5100-7-5001 PT1 AND FOUND PREVIOUSLY ACCOMPLISHED BY BRITANNIA AIRWAYS LIMITED REPAIR NR RS/757/53/727 ISSUE 1. RESDR FDEA200812035056Crease Beam · corrodedEXISTING REPAIR WAS FOUND ON RT CREASE BEAM INNER CHORD BETWEEN BS 760 AND BS 780. EXISTING REPAIR EVALUATED AS PER EO F-5100-75001 PT1 AND FOUND PREVIOUSLY ACCOMPLISHED BY BRITANNIA AIRWAYS LIMITED REPAIR NR RS/757/53/694 ISSUE 1. REPAIR IS CLASSIFIED AS MA
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