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 FDEA201108113216Skin · misrepairedRT WING INBD FLAP LOWER SKIN XIFH218 MISREPAIRED. REPAIR CARRIED OUT PER SRM 51-50-01 REPAIR 2 FIG.201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201108113215Skin · misrepairedRT WING INBD FLAP LOWER SKIN AT XIFH 188 MISREPAIRED. REPAIR CARRIED OUT PER SRM 51-50-01 REPAIR 2 FIG.201 REV 47. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV 112.SDR FDEA201108113214Skin · crackedLT WING L/E LOWER SKIN AT XOS 575, CRACKED. CARRIED OUT REPAIR AS PER EA 1-5740-143647. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV112.SDR FDEA201108113213Web · crackedCTR CARGO COMPARTMENT STA 1841 , WEB FOUND CRACKED AT LBL 40. REPAIR CARRIED OUT AS PER SRM 53-00-00 FIG.211 REV.47 AT CTR CARGO COMPT. STA.1841 WEB END CAP AT LBL 40. EO1-5100-7-5001 A5-PT1, REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV.112SDR FDEA201108113210Web · crackedCTR CARGO COMPARTMENT STA 1841, WEB FOUND CRACKED AT RBL 40. REMOVED AND NEW WEB FABRICATED AS PER DOUGLAS DWG AGA7170 REV T AND INSTALLED AT CTR CARGO COMPT. AS PER SRM 51-31-01 REV.47 EO1-5100-7-5001 A5-PT1, REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REVSDR FDEA201108113209Web · crackedBS 1841 WEB FOUND CRACKED AT RBL 47. NEW WEB FABRICATED AS PER DWG AGA7170 REV T AND INSTALLED. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV.112SDR FDEA201108113208Web · crackedCTR CARGO BAY STA 1841, WEB FOUND CRACKED LBL 8. REMOVED AND NEW WEB FABRICATED AS PER DWG AGA7170 REV T AND INSTALLED AS PER SRM 51-31-01 REV.47 EO1-5100-7-5001 A5-PT1, REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV.112SDR FDEA201108113207Web · crackedCTR CARGO BAY STA 1841, WEB FOUND CRACKED. AT LBL 13. REMOVED AND NEW WEB FABRICATED AS PER DWG AGA7170 REV T AND INSTALLED AS PER SRM 51-31-01 REV.47 EO1-5100-7-5001 A5-PT1, REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV.112SDR FDEA201108103171Frame · misrepairedFRAME REPAIR AT CABIN LT STA 535 9G NET LOWER SUPPORT YOKE FOUND NOT CARRIED OUT IAW DWG SG10530002. REPAIR CARRIED OUT PER DWG SG10530002 AND EA1-5310-143652. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201108103170Frame · misrepairedREPAIR AT CABIN LT STA 535 9G NET UPPER SUPPORT YOKE, FOUND NOT CARRIED OUT IAW DWG SG10530002. REMOVED AND NEW REPAIR CARRIED OUT PER DWG SG10530002 AND EA 1-5310-143652. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201108103173Skin · misrepairedREPAIR FOUND ON LT WING INBD L/E UPPER. FOUND NOT IAW SRM 57-40-02 REPAIR 8 FIG.201 REV 47. NEW REPAIR CARRIED OUT IAW SRM 57-40-02 REPAIR 8 FIG.201 REV.47. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201108103169Frame · dentedCABIN RT STA 1701 L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG.201 REPAIR 2 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201108103168Frame · dentedCABIN RT 1721 L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG.201 REPAIR 2 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA201108103167Frame · dentedCABIN RT STA 1741 L-11 FRAME FOUND DENTED. REPAIRED AS PER SRM 53-00-07 FIG.201 REPAIR 2 REV 47. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.SDR FDEA200911053856Fitting · damagedNR4 BANJO FITTING OF VERTICAL STAB FOUND EXISTING REPAIR ON LT SIDE UPPER FASTENER HOLE. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.SDR FDEA200911053855Fitting · damagedBANJO FITTING STA Y-2169 LT SIDE FWD FLANGE 02EA EXISTING FASTENERS HOLE FOUND OVERSIZED DURING REPAIR JUST ABOVE CARRY THROUGH CAP. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.SDR FDEA200910293721Fitting · wornHFEC OPEN HOLE INSP UNABLE TO BE CARRIED OUT ON FASTENER HOLE NR11 (COUNTING FROM LT SIDE) AT NR4 BANJO FITTING AFT STA 2164 DUE TO HOLE DAMAGED. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.SDR FDEA200910293720Fitting · gougedAFTER REMOVAL OF STRAP AT RT SIDE OF BANJO NR4 FOUND GOUGE MARK ON BANJO FITTING SURFACE. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.SDR FDEA200910273694Strap · gougedEMPENNAGE- UPON STRAP REMOVAL ON THE RT SIDE FOUND WITH GOUGE MARKS. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.SDR FDEA200910273693Angle · crackedUPON REMOVAL OF CRACKED ANGLE AT BANJO FITTING NR 4 AFT FOUND 8 EA HOLES WITH REPAIR BUSHING. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.SDR FDEA200910263661Fitting · crackedWHILE CARRYING OUT BANJO FITTING REPAIR PER MANUFACTURER INSTRUCTION, FOUND RT AFT BANJO FITTING CRACKED. REPAIR CARRIED OUT AS PER E.A. 1-5530-135612, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 108.SDR FDEA200910193611Frame · dentedCABIN - RT STA 1641, L-11 TO L-12 FRAME FOUND DENT. REPAIRED IAW SRM 53-00-07 FIG 201, REV 41. INITIAL INSP TO BE CARRIED OUT AT 14,500 FLT CYCLES AND SUBSEQUENT REPETITIVE INSPECTIONS AT EVERY 9,500 FLIGHT CYCLES IAW SRM 53-00-07, TABLE 201. REPAIR 2, REV SDR FDEA200910193610Frame · dentedCABIN - RT STA 1661, L-11 TO L-12 FOUND DENT. REPAIRED IAW SRM 53-00-07 FIG 201, REV 41. INITIAL INSP TO BE CARRIED OUT AT 14,500 FLIGHT CYCLES AND SUBSEQUENT REPETITIVE INSPECTIONS AT EVERY 9,500 FLIGHT CYCLES IAW SRM 53-00-07 TABLE 201, REPAIR 2 REV 41. SDR FDEA200910193609Frame · dentedCABIN - RT STA 1761, L-11 TO L-12 FOUND DENT. REPAIRED IAW SRM 53-00-07 FIG 201. REPAIR 2, REV 41. INITIAL INSP TO BE CARRIED OUT AT 14,500 FLIGHT CYCLES AND SUBSEQUENT REPETITIVE INSPECTIONS AT EVERY 9,500 FLIGHT CYCLES IAW SRM 53-00-07, TABLE 201, REPASDR FDEA200910193608Frame · chafedCABIN - LT STA 1781, L-11 TO L-12 FOUND CHAFED. REPAIRED IAW SRM 53-00-07 FIG.201. REPAIR 2 REV 41 INITIAL INSP TO BE CARRIED OUT AT 14,500 FLIGHT CYCLES AND SUBSEQUENT REPETITIVE INSP AT EVERY 9,500 FLIGHT CYCLES IAW SRM 53-00-07, TABLE 201. REPAIR 2, REV SDR FDEA200910193607Frame · dentedCABIN - LT STA 1761, L-11 TO L-12 FOUND DENT. REPAIRED IAW SRM 53-00-07 FIG 201. REPAIR 2 REV 41 INITIAL INSP TO BE CARRIED OUT AT 14,500 FLIGHT CYCLES AND SUBSEQUENT REPETITIVE INSPECTIONS AT EVERY 9,500 FLIGHT CYCLES IAW SRM 53-00-07, TABLE 201, REPAIR 2 SDR FDEA200910193606Doubler · crackedCTR LANDING GEAR WW, WWL LT FWD SIDE DOUBLER CRACKED. REMOVED IAW SRM 51-31-01 REV. 41. DOUBLER FABRICATED IAW DWG AEA0526 REV. NC. NEW DOUBLER INSTALLED IAW SRM 51-31-01 REV 41. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 108.SDR FDEA200910153590Fitting · crackedCRACK INDICATION FOUND APPROX 0.50" IN LENGTH DURING HFEC ON LT SIDE OF THE LWR VERTICAL STABILIZER FWD FLANGE OF UPPER REAR SPAR CAP. REPAIR CARRIED OUT IAW EA 1-5530-135612, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 108.SDR FDEA200909293432Controller · failedRECEIVED LEVEL-2 ANTI-SKID FAILURE ALERT WITH MASTER CAUTION ON TAKEOFF ROLL APPROX 70 KNOTS. ALL TEST PASSED IAW MM 32-45-01. INSPECT ALL WHEEL AND BRAKES NO DEFECT FOUND. CONSULT WITH MOCC FOR PRECAUTION REMOVED AND REPLACED ASCU AND RTS TEST PASSED IAW MSDR 08FDEA01785Frame · damagedMAIN DECK INTERIOR FUSELAGE AT LEFT STA 535 FRAME, LOWER SUPPORT YOKE, FOUND DAMAGED. REPAIRED AS PER DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR PER GMM 6-2- 100.SDR 08FDEA01784Frame · damagedMAIN DECK INTERIOR FUSELAGE AT LEFT STA 535 FRAME, UPPER SUPPORT YOKE FOUND DAMAGED. MAIN DECK INTERIOR FUSELAGE AT LEFT HAND STA 535, UPPER SUPPORT YOKE, DAMAGED FRAME REPAIRED AS PER FEDEX DRAWING SRZ-53-503. REPAIR CLASSIFIED AS MINOR PER GMM 6-2- 100.SDR 08FDEA01707Skin · corrodedMAIN DECK CENTER WING UPPER SKIN SURFACE AT STA 1341 X = 101 FOUND CORROSION. REPAIR CARRIED OUT AS PER EA 1-5710-113145, CLASSIFIED AS A MINOR REPAIR AS PER FEDEX GMM 6-2-100.SDR 08FDEA01616Skin · cracked14 FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. COMPLIED WITH E.A. 1-5710-113138, CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.SDR 08FDEA01615Skin · cracked16 EACH FASTENER HOLES FOUND WITH CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. COMPLIED WITH E.A. 1-5710-113137, CLASSIFIED AS MINOR REPAIR AS PER GMM 6-2-100.SDR 08FDEA01614Frame · damagedUPPER FUSELAGE INTERIOR FRAME AT RIGHT STA 1681 LONGERON 11 FOUND DAMAGED. UPPER FUSELAGE INTERIOR, DENT FRAME AT RT BS 1681 LONGERON 11 REPAIRED AS PER SRM 53-30-00. INITIAL INSPECTION AT 14,500 CYCLES AND REPETITIVE INSPECTION AT 9,500 CYCLES TO BE CARRISDR 08FDEA01613Support Fitting · crackedMAIN DECK CARGO DOOR NR 4 LOWER JAMB SUPPORT FITTING 'B' HOLE FOUND CRACK AT 1 O'CLOCK POSITION. MAIN DECK CARGO DOOR NR 4 LOWER JAMB CRACKED SUPPORT FITTING REMOVED AND REPLACED AS PER SRM 51-31-01. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR 08FDEA01610Skin · dentedLEFT WING INBOARD FLAP LOWER SURFACE CENTER LOWER SEGMENT FOUND DENT. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG 17 VOL I. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR 08FDEA01390Indication Sys · malfunctioned90 MINUTES INTO FLIGHT RECEIVED LATER FUEL IMBALANCE WITH FUEL CONTROLLER IN AUTO. RAN QRH AUTO CONTROLLER RESOLVED IMBALANCE OF TNK 14000 LBS HEAVY. APPROXIMATELY 10 MINUTES LATER FP/R FUEL LOG INDICATED A CHANGE OF 2000 LBS UNACCOUNTED FOR AND INCREASINSDR 06FDEA04123Skin · crackedRIGHT WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUTOUT BETWEEN STATION XORS = 683.4 AND XORS = 713.6 FOUND CRACK ON FASTENER HOLE LOCATED AT 3:30 POSITION (LOOKING FORWARD VIEW UP). RIGHT WING LOWER SKIN PANEL, OUTER WING ACCESS DOOR CUTOUT BETWEEN STASDR 06FDEA04122Skin Panel · crackedLEFT WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND XORS = 713.6 FOUND CRACK ON FASTENER HOLE LOCATED AT 1:30 POSITION (LOOKING FORWARD VIEW UP). LEFT WING LOWER SKIN PANELS, OUTER WING ACCESS DOOR CUTOUT BETWEEN STA XORS =SDR 06FDEA04106Skin · delaminatedLT WING INBD FLAP VANE INBD LOWER SURFACE FOUND DELAMINATION. REPAIRED AS PER FEDEX E.A. 1-5750-105562.SDR 06FDEA04083Hinge · corrodedRIGHT WING, (WING SIDE) OUTBOARD FLAP OUTBOARD HINGE ACTUATOR ATTACHMENT INBOARD LUG HOLE FOUND CORRODED. REPAIRED PER FEDEX E.A. 1-5750-105569.SDR 06FDEA04082Hinge · corrodedRIGHT WING, INBOARD FLAP OUTBOARD HINGE PIVOT POINT OUTBOARD LUG BORE HOLE FOUND CORRODED. REPAIR AS PER FEDEX E.A. 1-5750-105567.SDR 06FDEA04081Hinge · corrodedRIGHT WING, INBOARD FLAP OUTBOARD HINGE PIVOT POINT INBOARD LUG BORE HOLE FOUND CORRODED. REPAIRED PER FEDEX E.A. 1-5750-105567.SDR 06FDEA04080Hinge · corrodedLEFT WING, INBOARD FLAP OUTBOARD HINGE PIVOT POINT OUTBOARD LUG BORE HOLE FOUND CORRODED. CARRIED OUT REPAIR AS PER FEDEX E.A. 1-5750-105566.SDR 06FDEA04079Hinge · corrodedLEFT WING, INBOARD FLAP OUTBOARD HINGE PIVOT POINT INBOARD LUG BORE HOLE FOUND CORRODED. REPAIRED PER FEDEX E.A. 1-5750-105566.SDR 06FDEA04047Skin · corrodedCARGO CTR FUEL TANK UPPER PANEL (STA 1239, RH X=100) FOUND LOCK FASENER PERIPHERY CORRODED. MAIN DECK CARGO (STA 1239, RH X = 100) CENTER FUEL TANK UPPER PANEL CORROSION REMOVED AND REPROTECTED AS PER SRM 51-21-01 VOLUME II. ORIGINAL THICKNESS = 0.1848", SDR 06FDEA04053Fitting · corrodedCENTER LANDING GEAR RT TRUNNION SUPPORT FITTING FWD BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR RT 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 06FDEA04052Fitting · corrodedCENTER LANDING GEAR RT TRUNNION SUPPORT FITTING CTR BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR RT 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 06FDEA04051Fitting · corrodedCENTER LANDING GEAR RT TRUNNION SUPPORT FITTING AFT BORE HOLE FOUND CORROSION. REPAIR CARRIED OUT AT CENTER LANDING GEAR RT 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.
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