N628FE
Service difficulty reports · 234
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 = 'N628FE' 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 = 'N628FE' 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 06FDEA04050Fitting · corrodedCENTER LANDING GEAR LT TRUNNION SUPPORT FITTING AFT BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING BORE HOLE AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA04049Fitting · corrodedCENTER LANDING GEAR LT TRUNNION SUPPORT FITTING CTR BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING BORE HOLE AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA04048Support Fitting · dirtyCENTER LANDING GEAR LT TRUNNION SUPPORT FITTING FWD BORE HOLE FOUND STAIN. STAIN AT CENTER LANDING GEAR LT TRUNNION SUPPORT FITTING FWD BORE HOLE CLEANED UP AS PER SRM 53-40-00 FIGURE 15 VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA04046Trunnion · corrodedCENTER LANDING GEAR RT TRUNNION MATING SURFACE FOUND CORRODED. CENTER LANDING GEAR RIGHT TRUNNION MATING SURFACE CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIGURE 15 VOLUME I. FORWARD SIDE ORIGINAL THICKNESS = 2.477". REMOVED MATERIAL = 0SDR 06FDEA04045Trunnion · corrodedCENTER LANDING GEAR LT TRUNNION MATING SURFACE FOUND CORRODED. CENTER LANDING GEAR LEFT TRUNNION MATING SURFACE CORROSION REMOVED AND FOUND WITHIN LIMIT AS PER SRM 53-40-00 FIGURE 15 VOLUME I. FORWARD SIDE ORIGINAL THICKNESS = 2.485". REMOVED MATERIAL = 0SDR 06FDEA04018Longeron · corrodedCTR CARGO COMPARTMENT, STA 5-11, L52 FOUND CORROSION. CENTER CARGO COMPARTMENT, STA 5-11, LONGERON 52 REPAIRED AS PER FEDEX EA#1-5310-105561, TITLE:"FUSELAGE-LONGERON L-52 LEFT AT STATION 5-21, SRM SPLICE REPAIR CLARIFICATION" AND SRM 51-33-01 VOLUME II. SDR 06FDEA04019Frame · dentedM/D CARGO, INTERIOR FUSELAGE FOUND RT FRAME (STA 1781, L12) DENTED. MAIN DECK CARGO RIGHT FRAME (STA 1781, LONGERON 12) CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVSDR 06FDEA04012Splice · crackedM/D, STA 6-100 LONGERON 1R ON THE FORWARD SIDE OF THE INNER TRANSVERSE STRAP FOUND CRACK. CRACKED SPLICE AT MAIN DECK CARGO COMPARTMENT AT STA 6-100 LONGERON 1R. REMOVED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE MACHINED AS PER DRAWING A6A7112 AND INSTALLEDSDR 06FDEA04011Stringer Splice · crackedCTR CARGO COMPARTMENT, STA 5-113 L49L SPLICE FITTING FOUND CRACKED. CRACKED SPLICE FITTING AT CENTER CARGO COMPARTMENT STA 5-113 LONGERON 49L. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. NEW SPLICE FITTING FABRICATED AS PER DRAWING A5A7114. REPAIR SDR 06FDEA03977Frame · dentedCARGO LT FRAME (STA 1641, L12) FOUND DENT. MAIN DECK CARGO LEFT HAND FRAME (STA 1641, LONGERON 12) CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CAT B REPAIR INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,50SDR 06FDEA03976Frame · dentedCARGO LT FRAME (STA 1661, L12) FOUND DENT. MAIN DECK CARGO LEFT HAND FRAME (STA 1661, LONGERON 12) CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIONS AT 9,5SDR 06FDEA03975Frame · dentedCARGO LT FRAME (STA 1681, L11-13) FOUND DENT. MAIN DECK CARGO LEFT HAND FRAME (STA 1681, LONGERON 11 TO 13) CARRIED OUT REPAIR AS PER SRM 53-30-00 FIGURE 1 VOLUME I. DUE TO CAT B REPAIR, INITIAL INSPECTION REQUIRED AT 14,500 CYCLES WITH REPETITIVE INSPECTIOSDR 06FDEA03974Lanyard · disconnectedCABIN: SLIDE/RAFT AT R1 DOOR FOUND FIRING LANYAND DISCONNECTED WITH QUICK-DISCONNECT WHEN DOOR INTERIOR LWR COVER REMOVED FOR REPAIR. RECONNECTED R1 DOOR SLIDE/RAFT FIRING LANYAND AS PER AMM 25-61-06-4.SDR 06FDEA03973Lanyard · disconnectedCABIN: SLIDE/RAFT AT L1 DOOR FOUND FIRING LANYAND DISCONNECTED WITH QUICK-DISCONNECT WHEN DOOR INTERIOR LWR COVER REMOVED FOR REPAIR. RECONNECTED L1 DOOR SLIDE/RAFT FIRING LANYAND AS PER AMM 25-61-06-4.SDR 06FDEA03972Doubler · crackedLT WING, AT XOS 654 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03971Doubler · crackedLT WING, AT XOS 645 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03970Doubler · crackedLT WING, AT XOS 639 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03969Doubler · crackedLT WING, AT XOS 631 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03968Doubler · crackedLT WING, AT XOS 518 FIXED L/E BEADED DOUBLER FOUND CRACKED. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03950Doubler · crackedRT WING FIXED L/E BEADED DOUBLER FOUND CRACK AT XOS 665. RT WING FIXED LEADING EDGE BEADED DOUBLER AT XOS 665 REPAIRED AS PER SRM TR 57-5 57-10-00 FIGURE 25B VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03948Doubler · crackedRT WING FIXED L/E BEADED DOUBLER FOUND CRACK AT XOS 669. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03947Doubler · crackedRT WING FIXED L/E BEADED DOUBLER FOUND CRACK AT XORS 636-643. REPAIRED AS PER SRM 57-10-00 FIGURE 25 VOLUME I. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 06FDEA03946Stringer · crackedHFEC INSPECTION FOUND CRACK ON RT WING TANK AT THE END OF STRINGER 38. CRACK (STARTING FROM STOP DRILL HOLE TO INBOARD) ON EXISTING REPAIR DURING HFEC INSPECTION ON RT WING TANK AT THE END OF STRINGER 38 XORS 877 REPAIRED AS PER SRM 57-20-00 FIGURE 10 VSDR 06FDEA03945Stringer · crackedHFEC INSPECTION FOUND CRACK ON RT WING TANK AT THE END OF STRINGER 13. CARRIED OUT REPAIR AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03944Stringer · crackedHFEC INSPECTION FOUND CRACK ON LT WING TANK AT THE END OF STRINGER 9. CRACK ON LT WING TANK AT THE END OF STRINGER 9 AT XORS 819 REPAIRED AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 06FDEA03930Duct · crackedRT WING FIXED L/E TELESCOPING DUCT CUTOUT FOUND CRACK. REPAIRED AS PER FEDEX E.A. 1-5730-105556.SDR 06FDEA03929Duct · crackedLT WING FIXED L/E TELESCOPING DUCT CUTOUT FOUND CRACK. CARRIED OUT REPAIR AS PER FEDEX E.A. 1-5730-105557.SDR 05FDEA01403Frame · crackedDURING AIRPLANE'S CONVERSION FROM P TO F, FOUND CRACK 2.5 INCHES LONG ON FRAME LUG AT STA 1256 B/T L11 AND L12, RT SIDE. CUT OUT DAMAGED AREA AND REPAIR FRAME IAW SRM 53-30-00 FIG 2. CUT OUT DAMAGED AREA AND REPAIR FRAME IAW SRM 53-30-00 FIG 2.SDR 05FDEA00953Bulkhead · damagedDURING AIRPLANE'S CONVERSION FROM P TO F FOUND: EXISTING REPAIR ON BULKHEAD, AT STA 595, X=56 LT SIDE. NO ACTION REQUIRED. REPAIR IS IAW SRM 53-20-00 FIG 6 SHEET 5.SDR 05FDEA00949Structure · damagedDURING AIRPLANE'S CONVERSION FROM P TO F FOUND: EXISTING REPAIR AT FWD CARGO, FROM STA 775 TO STA 791, Z19, X= -117 LOWER FLOOR. NO ACTION REQUIRED: REPAIR IS IAW SRM 53-00-01, FIG 8, SHEET 5.SDR 05FDEA00957Structure · damagedDURING AIRPLANE'S CONVERSION FROM P TO F FOUND: REPAIR AT STA 990, STR 40-42 RT REQUIRES ENGINEERING EVALUATION TO DETERMINE WHETHER REPAIR IS MAJOR OR MINOR AND CONFORM TO APPLICABLE DATA. NO ACTION REQUIRED: REPAIR IS CONFORMED IAW SRE 53-50-00 FIG 7A.SDR 05FDEA00956Structure · damagedDURING AIRPLANE'S CONVERSION FROM P TO F FOUND: REPAIR AT STA 635, STR 43-46 LT REQUIRES ENGINEERING EVALUATION TO DETERMINE WHETHER REPAIR IS MAJOR OR MINOR AND CONFORM TO APPLICABLE DATA. NO ACTION REQUIRED: REPAIR IS CONFORMED IAW SRE 5320-00 FIG 2 SHEETSDR 05FDEA00955Structure · damagedDURING AIRPLANE'S CONVERSION FROM P TO F FOUND: REPAIR AT STA 5-53, STR 50-51 LT REQUIRES ENGINEERING EVALUATION TO DETERMINE WHETHER REPAIR IS MAJOR OR MINOR AND CONFORM TO APPLICABLE DATA. NO ACTION REQUIRED: REPAIR IS CONFORMED IAW SRE 53-20-00 FIG 6, SHSDR 05FDEA00954Structure · damagedDURING AIRPLANE'S CONVERSION FROM P TO F FOUND: REPAIR AT STA 1960, STR 40-42 LT REQUIRES ENGINEERING EVALUATION TO DETERMINE WHETHER REPAIR IS MAJOR OR MINOR AND CONFORM TO APPLICABLE DATA. NO ACTION REQUIRED: REPAIR IS CONFORMED IAW SRE 53-50-00 FIG 16.
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