N917FD
Service difficulty reports · 195
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 = 'N917FD' 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 = 'N917FD' 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 FDEA202204181245Floor Panel · damagedFLOOR PANEL NO 222MAF FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005. REF. ENGINEERING DISPOSITION OF RFTA NO: 02859-0207. P/N: N917FD-N00312-222MAF. B/N: 20353949. MAJOR REPAIR.SDR FDEA202204181244Floor Panel · damagedFLOOR PANEL NO 222MDF FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005. REF. ENGINEERING DISPOSITION OF RFTA NO: 02859-0207. P/N: N917FD-N00313-222MDF. B/N:20354003. MAJOR REPAIR.SDR FDEA202204181243Floor Panel · damagedFLOOR PANEL NO 221BF FOUND WORN REPLACED FLOOR PANEL PER FEDEX SRZ-25-005. REF. ENGINEERING DISPOSITION OF RFTA NO: 02859-0207.P/N: N917FD-N00308-221BF. B/N: 20353968. MAJOR REPAIR.SDR FDEA202204171240Skin · tornAPU INLET DOOR OUTBD LOWER EDGE IS BROKEN PERFORMED REPAIR PER SRM 53-80-31-2R,REPAIR 1,FIG. 201. MATERIAL P/N:EA9390 , B/N:JH1FAF7944. REV. 135.0. 17/1/22. REP. DIM.: 4" X 2". REP. LOC.: O/B LOWER FWD EDGE. MAJOR REPAIR.SDR FDEA202204061339None · noneEVALUATE REPLACED PART AT FRAME AT STA 231.25 BL-0 PER EO F-5100-7-5001 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-T0368488, FRAME AT STA 231.5 BTWN LBL-20, RBL-20, REPLACEMENT OF NON SATISFACTORY FRAME REPAIR. MAJOR REPAIRSDR FDEA202204061328None · noneEVALUATE EXISTING REPAIR AT FRAME AT STA 1000 BETWEEN STR 3L-3R PER EO F-5100-7-5001 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5310-150687B, FRAME SPLICE REPAIR AT STA 1000 BETWEEN S-5L & S-5R. MAJOR REPAIRSDR FDEA202204061327None · noneEVALUATE EXISTING REPAIR AT FLOOR BEAM AT STA 340 RBL-53-LBL-53 PER EO F-5100-7-5001 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A #F-5310-T0368523, FLOOR BEAM AT STA 345, BTW LBL 53 TO RBL 53, SRM REPAIR WITH MINOR DEVIATIONS MAJOR REPAIRSDR FDEA202204061304None · noneEVALUATE EXISTING REPAIR AT FRAME AT STA 1020 BETWEEN STR 3L-3R PER EO F-5100-7-5001 WORK ACCOMPLISHED PER FEDEX EA # F-5310-150688 B, EXISTING REPAIR AT FRAME STA 1020 B/T STR 5L -5R. MAJOR REPAIRSDR FDEA202204061303None · noneEVALUATE EXISTING REPAIR AT FLOOR BEAM AT STA 377 LBL-45 PER EO F-5100-7-5001 WORK ACCOMPLISHED PER FEDEX EA# F-5310-T0368447: EXISTING REPAIR AT STA 377, BETWEEN RBL17 AND LBL 45, TRACKING MAJOR REPAIRSDR FDEA202204061286None · noneEVALUATE EXISTING DOUBLER REPAIR AT FUSELAGE SKIN BETWEEN STA 1701-1720 STR 15L- 17L PER EO F-5100-7-5001 WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX EA # F-5330-T0368557, STA 1701-1720 S-15/S-16 L, EXISTING EXTERNAL REPAIR , DEVIATION FROM APPROVED DATA, SDR FDEA202204050849None · nonePDIS 917 33-20 3360 05APR22 CDG FACT U LOGPAGES:3301983 LEFT MAIN CABIN DOOR SLIDE (L1 SLIDE) LIGHT NOT ILLUMINATED ONCE ARMED. FACT 05APR22 00:14 CDG RELAMPED PER AMM 33SDR FDEA202110192579None · nonePDIS 917 25-60 2831 19OCT21 MAN OPEN U R1 ARMED (SLIDE) LIGHT DOES NOT ILLUMINATE WHEN R1 DOOR IS MECHANICALLY ARMED MEL 19OCT21 20:14 MAN U RELEASED FOR SERVICE PER MEL : 25-66-05-A CATEGORY : C EXPIRATION : 29OCT21 "MEL 25-66-05-A: R1 SDR FDEA202108051998Bulb · inoperativeEMERGENCY LIGHT DOOR 1L (SLIDE GND ILLUMINATION LT) INOP BULB REPLACED ACC AMM 33-51-06-2-1 REV 124.17. OPS TEST SATIS.SDR FDEA202101090053Test Switch · looseEMERGENCY LIGHT TEST SWITCH ABOVE DOOR 1L DOES NOT ILLUMINATE WHEN PUSHED AND EMERGENCY LIGHTS DO NOT ILLUMINATE WHEN TEST SWITCH PUSHED. IDENTIFIED PARTS SWITCH ASSEMBLY. FOUND WIRE AT NO CONNECTION AT SWITCH S10292 LOOSE. RECONNECTED AND FUNCTION TESTED, SDR FDEA202010042415Controller · malfunctionedAIRCRAFT DID NOT PRESSURIZE DURING CLIMB OUT IN AUTO 2 . LEVELED AT 10K WITH CABIN ALT EICAS WARNING. OUTFLOW VALVE INDICATED FULL OPEN . NO OTHER INDICATIONS ON EICAS. ACCOMPLISHED FIM 21-30 FT 815 AND FIM 21-3- FT 802 BOCK 1 FOUND CASDR FDEA202010042416Controller · failedAIRCRAFT DID NOT PRESSURIZE DURING CLIMB OUT IN AUTO 2. LEVELED AT 10K WITH CABIN ALT EICAS WARNING. OUTFLOW VALVE INDICATED FULL OPEN. NO OTHER INDICATIONS ON EICAS. ACCOMPLISHED FIM 21-30 FT 815 AND FIM 21-3- FT 802 BLOCK 1 FOUND CABIN ALT PRESS CONTROLLSDR FDEA2020052651043Attach Bracket · crackedLOOSE FASTENERS ON STRUT NR 2 AFT SAILBOAT FAIRING DIRECTLY ABOVE DRAIN TUBES FAIRING REMOVED IAW SRM 51-40-02 WORN FASTENER HOLES FOUND IN FAIRING SKIN AND SUPPORT STRUCTURE, FAIRING ATTACH BRACKET FOUND TO BE CRACKED. REPLACED AFT FAIRING SKIN, SUPPORT CHANNSDR FDEA2020052651042Scuff Plate · crackedDOOR 4R FORWARD SCUFF PLATE CRACKED. WELD REPAIRED DOOR 4R FORWARD SCUFF PLATE IAW DRAWING NR SR57-53-003.SDR FDEA202005180973Scuff Plate · crackedAFT SCUFF PLATE ,AT DOOR 2R LOWER FUSELAGE SKIN CUTOUT CRACKED . SCUFF PLATE REMOVED IAW SRM 51-40-02. SCUFF PLATE REPAIRED IAW FEDEX REPAIR DRAWING SR57-53-003. SCUFF PLATE INSTALLED IAW SRM 51-40-02.SDR FDEA202005180972Fairing · crackedPYLON NO.1 AFT FAIRING CRACKED AT HEATSHIELD JUST ABOVE DRAIN OUTLETS CRACKED FAIRING REMOVED IAW SRM 51-40-02, OVERSIZED HOLES FOUND ON FAIRING SUPPORT STRUCTURE, REPAIR CARRIED OUT IAW FEDEX EA # F-5430-T0353727 P1 TITLE NACELLES / PYLON- SKIN/ PLATES / SDR FDEA2020052641045Fitting · corrodedDUE TO FASTENER HOLE CORROSION DAMAGE, DOOR 4R UPPER FITTING PN 146N8761-16 REQUIRES REPLACEMENT. DOOR 4R UPPER FITTING PN 146N8761-16 REPLACED IAW DRAWING 146N8738, SRM 51-40-02 AND EA F-5310-T0354066 (P1) TITLE :FUSELAGE- MAINFRAME- DISCREPANT HOLES IN DOORSDR FDEA202005110918Frame · crackedNR 6 AFT FLAP TRACK FAIRING 672CB HAS DAMAGE ON FORWARD OUTBOARD FRAME. REPLACED FRAME IAW SRM 51-40-02 AND DRAWING 113N1752 ALSO REFER TO EA F-5720-T0353885 TITLE: WING-SECONDRY WING STRCT- NR 6 AFT FLAP TRACK FAIRING FRAME.SDR FDEA2020050860901Floor Panel · gougedFWD CARGO COMPARTMENT FLOOR PANEL BSTA 820 LBL 10 HAS MINOR GOUGE EVALUATE FOUND OUTSIDE SRM LIMITS AND CARRIED OUT PERMANENT REPAIR ON FLOOR PANEL 12 121CF 11" FROM L/H SIDE AND 25.5" FROM AFT EDGE BSTA 820 LBL 10 IAW DRAWING SR57-53- 001 AND SRM 51-40-02SDR FDEA2020050400867Floor Panel · damagedCABIN FLOOR BOARD 221AF TOP LAYER DAMAGED REPAIRED FLOOR BOARD 221AF IAW SRM 53-00-50 REV 129SDR FDEA2020050400865Floor Panel · damagedCABIN FLOOR BOARD # 221MBF TOP LAYER DAMAGED REPAIRED FLOOR PANEL 221MBF IAW SRM 53-00-50 REV 129SDR FDEA2020043090837Retainer · crackedTWO AREAS OF POSSIBLE CRACKS IN SEAL RETAINER FWD CARGO DOOR, CUTOUT LOWER CORNER AND 22" FROM LOWER AFT CORNER REPAIRED TWO AREAS ON FORWARD CARGO DOOR SEAL RETAINER IAW EA F-5340- T0353716 PT1. THIS IS A MINOR REPAIRSDR FDEA2020043090832Bracket · corrodedEVIDENCE OF CORROSION ON AILERON CABLE GUIDE BRACKET IN R/H MLG WHEEL WELL FORWARD WALL OUTBOARD SIDE. .CABLE GUIDE BRACKET REPLACED IAW SRM 51-40-02 BOEING DRAWING NUMBERS 274N1048 AND 274N1055.SDR FDEA2020043080812Skin · dentedDENT ON FUSELAGE SKIN AT BSTA 1691 BETWEEN STR 14-15 L/H EVALUATED DENT OF FUSELAGE SKIN BS1691 BETWEEN STR 14-15 L/H IAW SRM 53-00-01-1A AND FOUND TO BE OUTSIDE SRM LIMITS DUE TO PROXIMITY TO ADJACENT LAP JOINT. REFER TO FEDEX EA F-5330-T0353565 TITLE FUSELSDR FDEA2020051570934Attach Bracket · crackedPYLON #1 AFT FAIRING AFT HEATSHIELD ATTACH BRACKETS CRACKED REPLACED CRACKED BRACKETS IAW BOEING DRAWING # #313N052 AND SRM 51-40-02SDR FDEA2020050460864Floor Panel · damagedUPPER DECK FLOOR PANEL DAMAGED BSTA 1681 LBL 60.20 REPAIRED UPPER DECK FLOOR PANEL IAW SRM 53-00-50 REV 129SDR FDEA2020043060859Floor Panel · dentedFLOOR PANEL DAMAGED BSTA 1681 LBL 12" REPAIRED FLOOR PANLE IAW SRM 53-00-50 REV 129SDR FDEA2020043060858Floor Panel · dentedFLOOR PANEL DAMAGED BSTA 1681 LBL 12" REPAIRED FLOOR PANEL IAW SRM 53-00-50 REV 129SDR FDEA2020051850974Floorbeam · corrodedEVIDENCE OF CORROSION ON FLOORBEAM UPPER SURFACE BS 365 RBL46 CORROSION REMOVED IAW SRM 51-10-02 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-51-1A. AREA REPAIRED IAW EA F-5310-T0353724.SDR FDEA2020051540896Fill Port · corrodedR/H OVERWING FILL PORT HAS EVIDENCE OF CORROSION REMOVED CORROSION AT R/H WING FILL PORT AREA IAW SRM 51-10-02 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 57-20-01-1A REPAIRED R/H FILL PORT AREA IAW SRM 57-20-01 REPAIR 7 THIS IS A MAJOR REPAIR .SDR FDEA2020051540895Fill Port · corrodedL/H OVERWING FILL PORT HAS EVIDENCE OF CORROSION REMOVED CORROSION AT L/H WING FILL PORT AREA IAW SRM 51-10-02 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 57-20-01-1A. REPAIRED L/H FILL PORT AREA IAW SRM 57-20-01 REPAIR 7 THIS IS A MAJOR REPAIR.SDR FDEA2020043040856Floor Panel · dentedFLOOR PANEL AT BSTA 560-680 HAS LARGE DENT ON TOP SKIN REPAIRED FLOOR PANEL IAW SRM 53-00-50 REV 129SDR FDEA2020050490866Floor Panel · damagedFORWARD CABIN FLOOR BOARDS # 222 MAF, FOUND TOP LAYER OF BOARDS DAMAGES REPAIRED FLOOR PANEL 222MAF IAW SRM 53-00-50 REV 129SDR FDEA2020042790781Angle · corrodedCORROSION @ ANGLE AFT OF BULK CARGO B/S 1715 RBL 25 STR 17 EVALUATED CORRODED STIFFENER ANGLE AT BS 1715 RBL 25 IAW SRM 53-60-51-1A AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STIFFENER ANGLE AT BS 1715 RBL 25 IAW SRM 51-40-02 AND BOEING DRAWING #SDR FDEA2020060381118Floorbeam · corrodedEVIDENCE OF CORROSION ON FLOORBEAM, UPPER CHORD, LOWER SURFACE, AT BS1681 RBL 24 ADJACENT TO ANCHOR NUTPLATE. CORROSION REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-51-1A. PREVIOUS UPPER CHORD REPLACEMENT REPLACED IAW EA F-5310-T0353625 P1 TITLE: FUSDR FDEA2020051180909Bulkhead · gougedGOUGE FOUND ON NLG WHEEL WELL FWD BULKHEAD AT BS 263 NEAR BL0 DAMAGE REMOVED IAW SRM 53-10-08-1A AND FOUND TO BE OUTSIDE LIMITS, ORIGINAL MATERIAL THICKNESS .090" MATERIAL REMOVED 0.030" MAX ALLOWABLE 0.009". REPAIR CARRIED OUT IAW FEDEX EA # F-5330-T0353SDR FDEA2020050480863Seat Track · corrodedCORROSION FOUND ON CABIN FLOOR SEAT TRACK @ BSTA 1180-1195 RBS 45.5 CORROSION REMOVED IAW SRM 51-10-02 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-00-52- 1A. SEAT TRACK REPLACED FROM BS 1180 TO BS 1280 RBL 45.5 IAW SRM 51-40-02 AND BOEING DRAWING # 146N51SDR FDEA2020042780803Stiffener · corrodedSHEAR DECK STIFFENER AT BS1706 RBL 51.50 WL 208 CORRODED BEYOND LIMITS EVALUATED CORRODED STIFFENER ANGLE AT BS 1706 RBL 51.5 IAW SRM 53-60-51-1A AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED STIFFENER ANGLE AT BS 1706 RBL 51.5 IAW SRM 51-40-02 AND SDR FDEA2020042780780Stiffener · corrodedEVIDENCE OF CORROSION ON SHEAR DECK STIFFENER AT BS1715 BETWEEN RBL33 AND RBL 39 WL 208 REMOVED CORRODED SHEAR DECK STIFFENER AT BS 1715 RBL 33 TO RBL 39 AND FOUND TO BE OUTSIDE LIMITS IAW SRM 53-60-51-1A. REPLACED STIFFENER IAW SRM 51-40-02.AND BOEING DRSDR FDEA2020042780779Stiffener · corrodedEVIDENCE OF CORROSION ON SHEAR DECK STIFFENER AT BS1715 RBL10 - RBL16 WL208 REMOVED CORRODED STIFFENER AT BS 1715 RBL 10 - RBL 16 AND FOUND CORROSION TO BE BEYOND LIMITS IAW SRM 53-60-51-1A. STIFFENER REPLACED IAW SRM 51-40-02 AND BOEING DRAWING # 146N52SDR FDEA2020052631046Slat · corrodedLT WING NR 1 LEADING EDGE SLAT HEAVILY CORRODED. REPLACED NR 1 LEADING EDGE SLAT IAW AMM 27-81-02 P/N OFF 114N4002-133 S/N OFF A1-0087 P/N ON 114N4002-153 S/N ON A1-0622 TAG NR 34G492.SDR FDEA2020032342642Valve · leakingPDIS 917 29-30 0753 14OCT19 TLV OPEN U LOGPAGES:3025445 STARTED BOTH ENGINES WITH BRAKES SET. ON SELECTION OF AFTER START FLAPS 5, MASTER CAUTION, R HYD SYS PRESS, R HYD RSVR PRESS, R HYD QTY HYD QTY L 0.94 - C 1.01 - R 0.0 RF HYD PRESS L 29SDR FDEA2019101742642Valve · leakingSTARTED BOTH ENGINES WITH BRAKES SET. ON SELECTION OF AFTER START FLAPS 5, MASTER CAUTION, R HYD SYS PRESS, R HYD RSVR PRESS, R HYD QTY HYD QTY L 0.94 - C 1.01 - R 0.0 RF HYD PRESS L 2910 - C 3110 - R 30SDR FDEA201905151074Skin · damagedMDIS 917 57-50 0329 14MAY19 LGG OPEN U REF WRI: 0500/0327. DURING BIRD STRIKE INSPECTION, FOUND LT LEADING EDGE SLAT NR 5 DAMAGED. SLAT REQUIRES REPLACEMENT. R&R NR 5 LEADING EDGE SLAT IAW 27-81-01-4. OPS CHECK SATIS. A/C OK TO CONTINUE.SDR FDEA201904080774Retainer · corrodedEVIDENCE OF CORROSION ON RH MLG WHEEL WELL CUT OUT FWD EDGE SEAL RETAINER REMOVED CORROSION IAW SRM 51-10-02 REPAIRED AREA IAW E.A. # F-5350-T0346239 P1SDR FDEA201901100085Unknown · malfunctionedPDIS 917 22-10 0031 10JAN19 TLV OPEN U LOGPAGES:3019020 UNCOMMANDED NOSE DOWN. A/P CENTER, FL 210 PASSING FL 220, 4500 FPM RATE OF DESCENT, SPEED WINDOW CLOSED, NO A/P FAULT LIGHT. A/P DISCONECTED. VERY HEAVY YOKE ON PULL OUT MN. MEL 10JAN19 17:13 TLV U RELEAS
Back to N917FD