N903FD
Service difficulty reports · 162
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 = 'N903FD' 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 = 'N903FD' 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 FDEA201107262983Skin · dentedDENT EXTERIOR FUSELAGE SKIN AT STA 1559 BETWEEN S25-26R. DENT OUT OF LIMITS IAW SRM 53-00-01, FIG 101. CUT OUT DAMAGED SKIN, FABRICATED REPAIR PARTS AND INSTALLED IAW EA F-5330-136791.SDR FDEA201101280403Module · failedAT T/O, NOSE STRUT EXTENSION EVERYTHING NORMAL HAD AURAL FIRE WARNING BELL ON BOTH OVERHEAD SPEAKERS WITH NO OTHER INDICATIONS. LIGHTS TESTED NORMAL. BELL WENT OUT WHEN BOTH OVERHEAD SPKR C/B'S PULLED. UNEVENTFUL RETURN. PERFORMED PSEU BITE IAW FIM 32-09-0SDR FDEA201101280402Module · malfunctionedNLG STRUT EXTENSION, AURAL FIRE WARNING BELL ON BOTH OVERHEAD SPEAKERS WITH NO OTHER INDICATIONS. LIGHTS TESTED NORMAL. BELL WENT OUT AFTER BOTH OVERHEAD SPEAKER C/B'S PULLED. UNEVENTFUL RETURN. PERFORMED PSEU BITE IAW FIM 32-09-03/101. NO FAULTS. PERFSDR FDEA200910143557Unknown · power lossWHEN SELECTING ACFT PWR (APU) ON THE GND, THE PWR SHIFT REJECTED THE APU PWR, THE APU FAULTED AND SHUTDOWN. QRH PROCEDURE FOLLOWED AND APU RESTARTED SUCCESSFULLY AND THE AC ACCEPTED THE APU PWR. AFTER TAKEOFF THEN BEGAN TO EXPERIENCE NUMEROUS ELECTRICAL ANSDR FDEA200910033464Circuit Board · failedAPU FAULTED, RAN QRH CHECKLIST. APU FAULT LIGHT REMAINED ON. SINCE SINGLE GEN OPS RETURNED TO ICT. CREW REPORTED THAT APU DID AUTO SHUTDOWN AND IAW CHECKLIST THEY WERE NOT DIRECTED TO TAKE SWITCH TO OFF. THEY TRIED TO RESTART WITH NO LUCK. WHEN ACFT ARRIVSDR FDEA200909223348Gcu · damagedON CLIMBOUT ELECTRICAL SYSTEM STARTED TO "FADE" IN AND OUT. SEEMED TO BE THE LT SIDE ELECTRICAL, AUTOPILOTS AND AUTO THROTTLES BECAME INTERMITTENT. WHEN A/P WOULD BE WORKING IT HAD A PRONOUNCED BUMP IN PITCH LIKE AIR IN HYD SYS. CAPT'S FMC TIMED OUT AND WSDR FDEA200909173326Control Panel · failedON CLIMB OUT ICT, CTR A/P FAILED. (HEAVY PITCH PULLS) RETURNED TO ICT C/W QRH. ORIGINAL PLAN DATE WAS ENTERED. RELEASED FOR SERVICE IAW MEL: 22-10-01-C CATEGORY: B EXPIRATION: 20SEP09 "MEL 22-10-01-C: ALL AUTOPILOTS INOP. - ACFT NOT C ATII - NO RVSM OSDR FDEA200906292387Thrust Reverser · inoperativeL REV ISLN VAL ALERT AT 80 KTS. REJECTED TAKEOFF. RELEASED FOR SERVICE IAW MEL/CDL: 78-31-01-01. CATEGORY: C EXPIRATION: 10JUL09 "MEL 78-31-01-01: LT ENGINE THRUST REVERSER INOP. REVERSER SECURED IN FWD THURST POSITION." INSTALLED BOTH EICAS COMPUTERS REFSDR FDEA200906102014Restrictor Valve · malfunctionedREJECTED TAKE OFF AT 75KT FOR LT REVERSER ISOLATION VALVE EICAS MSG. COMPLIED WITH QRH PROCEDURES, RETURNED TO GATE. ( STATUS MSG "L REV ISLN VAL") FAULT CODE: 78-34-XC. ACFT RELEASED FOR SERVICE IAW MEL/CDL: 78-31-01-01. FOUND BOTH TRANS COWL GAPS OUT OF LSDR FDEA200809163906Relay · malfunctionedL REV AMBER LIGHT ON RAN QRH NO YAW OR ADVERSE CONDITIONS. ACFT RELEASED FOR SERVICE PER MEL/CDL: 78-36-01 CATEGORY: C EXPIRATION: 26SEP08 MEL 78-36-01: LEFT ENGINE REVERSER UNLOCK INDICATION INOP. REVERSER DEACTIVATED IN FORWARD THRUST POSITION. "A/C CAT SDR 08FDEA03906Thrust Reverser · malfunctionedL REV AMBER LIGHT ON RAN QRH NO YAW OR ADVERSE CONDITIONS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-36-01 CATEGORY: C EXPIRATION: 26SEP08 MEL 78-36-01: LEFT ENGINE REVERSER UNLOCK INDICATION INOP. REVERSER DEACTIVATED IN FORWARD THRUST POSITION." "A/C CAT ASDR 08FDEA02346None · noneACCOMPLISHED BOEING SB 757-54-0035, R2, PARA. 3, PART 3, STRUCTURE CHANGES FOR THE NR 2 STRUT, EXCEPT STEO Q, PANEL 5, PER FEDEX EA F-5450-108907, DATED 11 OCT 2007. COMPLIED WITH FEDEX EA F-5450-108907A, DATED 28 MAY 2008 ON W/C T F-5450-108907A, WRI 5450017SDR 08FDEA02345None · noneACCOMPLISH SB 757-54-0035, R2, PARA 3, PART 2; WING STRUCTURE CHANGES FOR THE NR 2 STRUT AND RT WING PER EA F-5450-108907, DATED 11 OCT 2007. ACCOMPLISHED SB 757-54-0035, PART 2, ON NR 2 STRUT, AS PER EA F-5450-108907A, DATED 28 MAY 2008. PER EA, SCHEDULE EOSDR 08FDEA02077Skin Panel · gougedRIGHT WING T/E O/B FLAP NOSE SKIN TOP SIDE HAS GOUGE. REMOVED RIGHT WING T/E FLAP NOSE SKIN IAW SRM 51-40-02. RECEIVED NEW PART P/N 113N3500Y28. INSTALLED NEW SKIN IAW SRM 51-40-02.SDR 08FDEA02000Skin · dentedEXTERNAL FUSELAGE LOWER SKIN, APPROX BS 255, STR 27L, DENT WITH GOUGE. ACCOMPLISHED A MAJOR REPAIR IAW EA F-5330-110861, WITH A RELEASE DATE OF 5/9/08. THERE IS NO FOLLOW UP TRACKING OR REPETITIVE INSPECTIONS REQUIRED FROM THIS REPAIR.SDR 08FDEA01337Seat Track · wornSEAT TRACK DAMAGED AT BS 640, LBL 24.75, MAIN CABIN. REMOVED SEAT TRACK ASSY IAW SRM 51-40-02. FABRICATED REPLACEMENT SEAT TRACK ASSY FROM BAC1520-792/24 IAW SRM 53-30-02. INSTALLED REPLACEMENT SEAT TRACK ASSY, FROM BS 440-640, LBL 24.75, IAW SRM 51-40-02. SDR 08FDEA01202Channel · corrodedU CHANNEL ON MCD, AT STA. 341, WL 208, LBL 21 TO 31 IS CORRODED. REMOVED CORROSION, L=9.2", W= 1.8", D= .008", ORIGINAL MATERIAL THICKNESS .054". FOUND TO BE OUT OF SRM 53-00-51, FIG 101, DETAIL III LIMITS. REMOVED U CHANNEL IAW SRM 51-40-02. FABRICATED RESDR 08FDEA01201Attach Bracket · corrodedNR 1 CARGO DOOR, CUT OUT LOWER SILL, THRESHOLD TIE DOWN ATTACH BRACKET, THIRD ONE FROM FWD END HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02, L= 1.75", W= .625", D= .009", ORIGINAL MATERIAL THICKNESS .063". FOUND TO BE OUT OF SRM 53-30-15, FIG 101, DETAISDR 08FDEA01167Panel · corrodedAFT CARGO FLOOR, SIDE PANEL (THRESHOLD AREA) HAS SURFACE CORROSION BETWEEN STA 1380-1440. REMOVED CORROSION, L= 3", W= 3", D= .020", FOUND TO BE OUT OF LIMITS PER SRM 53-60-35 WHICH REFERS ALLOWABLE DAMAGE TO SRM 53-00-53, FIGURE 101, DETAIL V. REMOVED SIDE SDR 08FDEA01088Intercostal · corrodedAFT PIT, LOWER FLANGE OF INTERCOSTAL AT STA 1402, RBL 2.90 IS CORRODED. REMOVED CORROSION, L=3.9", W= .75", D= .012", ORIGINAL MATERIAL THICKNESS WAS .040". INTERCOSTAL FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04, FIG 101, DETAIL II LIMITS. REMOVED INTERCOSTSDR 08FDEA00925Splice · corrodedUPON REMOVAL OF INTERCOSTAL AT STA 1400, LBL 2, FOUND CORROSION ON BUTT SPLICE STRAP. REMOVED CORROSION IAW SRM 51-10-02, L= 1.5", W= 1.1", D=.030" SRM DOES NOT PROVIDE ALLOWABLE DAMAGE LIMITS FOR THIS PART, CONTACTED ENGINEERING. PER EA F-5330-110824: TRIMMSDR 08FDEA00924Floor Support · corrodedAFT CARGO FLOOR SUPPORT AT BETWEEN STA 1320-1340, RBL 12, HAS CORROSION AROUND NUT PLATE HOLES. REMOVED CORROSION IAW SRM 51-10-02, L= 2", W= 1", D= .013", ORIGINAL MATERIAL THICKNESS .063". FOUND TO BE OUT OF SRM 53-00-53, FIG 101, SHEET 2 LIMITS. FABRICATSDR 08FDEA00687Channel · corrodedMAIN CARGO DECK FLOOR CHANNEL BETWEEN STA 324 TO 333, LBL 21, WL 208 HAS CORROSION. REMOVED CORROSION FROM CHANNEL IAW SRM 51-10-02, L= 8.5 INCHES, W= 2.4 INCHES, D= .007 INCH, ORIGINAL MATERIAL THICKNESS 0.49 INCH. FOUND TO BE OUT OF SRM 53-00-51, FIG 101SDR 08FDEA00685Crease Beam · corrodedMAIN CARGO DECK FLOOR, CREASE BEAM WEB CORRODED AT STA 1360, RBL 60, WL 208. REMOVED CORROSION IAW SRM 51-10-02, L= 2.5, W= 2.5, D= 0.031, ORIGINAL MATERIAL THICKNESS 0.040. FOUND TO BE OUT OF SRM 53-60-13, FIG 101, DETAIL III LIMITS. REMOVED WEB IAW SRM 51SDR 08FDEA00684Channel · corrodedMAIN CARGO DECK FLOOR, U CHANNEL, BETWEEN STA 310 TO 324, LBL 21, WL 208, HAS CORROSION. REMOVED CORROSION FROM U CHANNEL IAW SRM 51-10-02, L= 2.3 FT, W= 2.0 INCHES, D= .015 INCHES, ORIGINAL MATERIAL THICKNESS .054", FOUND TO BE OUT OF SRM 53-00-51, FIG 101SDR 08FDEA00683Skin · crackedRT WING NR 9 L/E SLAT HAS A CRACK PROPAGATING FROM RIVET HOLE, I/B SKIN FWD OF I/B SLAT TRACK. REMOVED I/B SKIN FROM NR 9 L/E SLAT IAW SRM 51-40-02. FABRICATED NEW REPAIR SKIN ON MAE TRAVELER NR T8/719344 FROM 7075-T6 .050C. INSTALLED NEW REPAIR SKIN IAW SRSDR 08FDEA00672Floor Support · corrodedFLOOR SUPPORT FROM STATION 720 TO 740, LBL 60, WL208, HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF SRM 53-00-51, FIG 101, DETAIL III LIMITS, L= 8 INCH, W= 2 INCH, D= 0.15 INCH, ORIGINAL MATERIAL THICKNESS .056 INCH. FABRICATED NEW FLOOR SUPPORT ON MASDR 08FDEA00671Floor Support · corrodedFLOOR SUPPORT FROM STATION 720 TO 740, LBL60, WL208, HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF SRM 53-00-51, FIG 101, DETAIL III LIMITS, L= 8 INCH, W= 2 INCH, D= 0.15 INCH, ORIGINAL MATERIAL THICKNESS .056". FABRICATED NEW FLOOR SUPPORT ON MAE TRASDR 08FDEA00670Floor Support · corrodedFLOOR SUPPORT BY L2 DOOR, BETWEEN STATION 680 TO 700, LBL 60, WL 208 HAS CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF SRM 53-00-51, FIGURE 101, DETAIL III LIMITS, L=1.5 INCH, W= 1 INCH, D= 100 PERCENT. FABRICATED NEW SUPPORT ON MAE TRAVELER NR T7/71336SDR 08FDEA00669Crease Beam · corrodedCREASE BEAM BY L2 DOOR, FROM STATION 660 TO 740, LBL60, WL 208 HAS SEVERAL AREAS OF CORROSION. REMOVED CORROSION FROM CREASE BEAM, L= 2", W= 1", D= 100 PERCENT, EXFOLIATED COMPLETELY THROUGH, BEYOND SRM 53-30-15, FIG 101, DETAIL IV LIMITS. REMOVED AND REPLACSDR 08FDEA00637Floor Support · corrodedAFT CARGO COMPARTMENT AT STA 1400, LBL 2, THE FLOOR SUPPORT WEB IS CORRODED. REMOVED CORROSION, AREA IS L = 2", W = 1", D = 100 PERCENT OF MATERIAL THICKNESS. CORROSION IS OUT OF SRM 53-00-51, FIG 101, DETAIL III LIMITS. REMOVED WEB FROM STA 1400 TO 1420 IASDR 08FDEA00636Floorbeam · corrodedMAIN CARGO DECK FLOORBEAM AT STA. 700, LBL 58 HAS CORROSION. REMOVED CORROSION, AREA IS L=8", W=2", D=.035". ORIGINAL MATERIAL THICKNESS, 0.140" AFTER REWORK, 0.105', FOUND TO BE OUT OF SRM 53-00-51, FIG 101, DETAIL III LIMITS. REMOVED DAMAGED AREA IAW SRSDR 08FDEA00617Floor Support · corrodedFLOOR SUPPORT BY THE L2 DOOR, STA 700-720, LBL 60, WL208 HAS CORROSION. REMOVED CORROSION FROM FLOOR SUPPORT, L=12.0, W=1.7, D=0.015, ORIGINAL MATERIAL THICKNESS = 0.063. FOUND TO BE OUT OF SRM 53-00-51, FIG 101, DETAIL II AND III LIMITS. REMOVED AND REPLACESDR 08FDEA00578Seat Track · damagedSEAT TRACK DAMAGED AT STA 640, LBL 45.50, WL 208. REMOVED SEAT TRACK, FABRICATED NEW SEAT TRACK FROM MATERIAL: BAC 1520-792/24, LOCATED AND DRILLED, TREATED, PRIMED AND INSTALLED SEAT TRACK IAW SRM'S: 51-40-02, 53-30-52, 51-40-05 AND 51-20-01.SDR 08FDEA00577Access Panel · corrodedWING FUEL PANEL 542BB HAS SURFACE/FRETTING CORROSION. REMOVED CORROSION FROM PANEL 542BB, FOUND TO BE OUT OF SRM 57-20-01, SECTION A-A, DETAIL I LIMITS. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-118.SDR 08FDEA00576Access Panel · corrodedWING FUEL PANEL 541DB HAS SURFACE/FRETTING CORROSION. REMOVED CORROSION, FOUND TO BE OUT OF SRM 57-20-01, SECTION A-A, DETAIL I LIMITS. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116.SDR 08FDEA00541Panel · corrodedWING FUEL PANEL 541LB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 541LB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116, ALTERNATE PN: 112N6101-1.SDR 08FDEA00540Panel · corrodedWING FUEL PANEL 641JB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 641JB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-119.SDR 08FDEA00539Panel · corrodedWING FUEL PANEL 641KB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 641KB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116.SDR 08FDEA00538Access Panel · corrodedWING FUEL PANEL 641GB HAS SURFACE CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL.SDR 08FDEA00537Panel · corrodedWING FUEL PANEL 541EB HAS SURFACE FRETTING CORROSION. WING FUEL PANEL 541EB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-119.SDR 08FDEA00536Panel · corrodedWING FUEL PANEL 642AB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 642AB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116.SDR 08FDEA00535Panel · corrodedWING FUEL PANEL 642CB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 642CB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-117.SDR 08FDEA00534Panel · corrodedWING FUEL PANEL 642DB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 642DB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-117.SDR 08FDEA00533Panel · corrodedWING FUEL PANEL 641DB HAS SURFACE CORROSION. WING FUEL PANEL 641DB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-116.SDR 08FDEA00532Panel · corrodedWING FUEL PANEL 642BB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 642BB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-118.SDR 08FDEA00531Access Panel · corrodedWING FUEL PANEL 641MB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 641MB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 112N6101-5.SDR 08FDEA00530Access Panel · corrodedWING FUEL PANEL 641EB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 641EB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 112N6101-5.SDR 08FDEA00529Access Panel · corrodedWING FUEL PANEL 643AB HAS SURFACE/FRETTING CORROSION. WING FUEL PANEL 643AB CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01, SECTION A-A OF DETAIL I. ORDERED AND RECEIVED NEW PANEL, PN: 10-60031-120.SDR 08FDEA00467Panel · corrodedNR 2 PYLON PANEL 444BL IS GOUGED IN 2 PLACES AND HAS SURFACE CORROSION. REMOVED CORROSION IAW SRM 54-50-71. ORIGINAL MATERIAL THICKNESS .063. L=1.0", W=.50", D=.011". FOUND TO BE OUT OF SRM 54-50-71, FIG 101 LIMITS, 10 PERCENT MATERIAL LOSS. FABRICATED NE
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