N118FE, cancelled Oct 31, 2002
Service difficulty reports · 29
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 = 'N118FE' AND deregistration_id = 'N118FE-2002-10-31' 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 = 'N118FE' AND deregistration_id = 'N118FE-2002-10-31' 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 01FDEA00391Stringer · crackedAT BS 400 STR 1, 2R & 3L ARE CRACKED AT FASTENER COMMON TO STR AND FRAME. REMOVED AND REPLACED STRINGERS PER IAW FEDEX EA 7-5310-57956.SDR 00FDEA00718Valve · damagedRED GEAR DOOR LIGHT AND AMBER NOSE GEAR DOOR LIGHT REMAIN ON. ASSOCIATED AIR NOISE AND VIB FELT IN NOSE GEAR AREA. RED TAB PROC AND CYCLE GEAR. *S/D* REMOVED AND REPLACED NOSE STRUT CHARGING VALVE AND SERVICED WITH FLUID AND NITROGEN. PER GEAR RETRACTION SDR 00FDEA00676Valve · malfunctionedAFT T/O BRING RT PACK ON, TURNED NR 3 BLD ON AND RT PACK ON. AFT COMING ON A LOUD BOOMING NOISE HEARD AND MOMENTARY PRESS SPIKE IN CABIN. *S/D* REMOVED AND REPLACED NR 3 ENG BLEED AIR SHUTOFF VALVE. REMOVED AND REPLACED NR 3 ENG HIGH PRESS MODULATING AND SSDR 00FDEA00565Control Cable · out of adjON T/O, LANDING GEAR SELECTED UP, GEAR CAME UP WITH VIB AFT GREEN/RED GEAR IND WENT OUT WITH THE EXCEPTION OF THE RED DOOR LIGHT ON FWD PNL (NOSE). COMPLIED WITH RED TABS. A/C RELEASED FOR SERVICE PER MEL. *S/D* ADJUSTED NOSE GEAR DOORS PER MM 32-22-1. ADSDR 99FDEA00292Connector · dirty99-177 - LEFT LANDING GEAR DOOR LIGHT IND UNSAFE. AFT CYCLING GEAR, RED LIGHT EXTINGUISHED. CK LEFT DOOR SWITCH ADJUSTMENT PER MM 32-62-011-4. CLEANED AND SECURED CONNNECTOR. DOOR AND LIGHT CHECK NORMAL.SDR 99FDEA00071Skin · crackedLEFT SIDE OF FUSELAGE BS 1150 3 ABOVE STR S4L SHEAR FASTENER HEAD AND SKIN CRACK. REPAIRED PER SRM 53-30-3 FIG 13A.SDR 98FDEA00654Skin · corrodedNR 273 BULGING SKIN AT BS 340-342, RBL 18, WL 148. ** S/D ** REPAIRED SKIN AT BS 338, RBL 21, WL 148 IAW FEDEX SRM 53-30-03.SDR 98FDEA00617Chord · corrodedCORROSION (C-53-100-01,1) ON BS 351.2 FRAME BETWEEN STR 26 AND 27 LT. *S/D* REMOVED AND REPLACED BS 351.2 LOWER REINFORCEMENT CHORD PER FEDEX SRM 51-30-2.SDR 98FDEA0583Frame · corrodedPAE - NR 0546 - CORROSION (C53-100-010) ON E/E DOOR FRAME AT BS 423, RBL 4 - LBL 4, WL 148. (X)SDR 98FDEA00583Frame · corrodedNR 546 CORROSION (C53-100-010) ON E&E DOOR FRAME AT BS 423, RBL 4-LBL 4, WL 148. ** S/D ** R&R E & E DOOR FRAME AT BS 423, WL 148 PER FEDEX SRM 51-30-2 & FEDEX SRM 51-10-1.SDR 98FDEA00536Beam · crackedNR 0072 AFT CARGO DOOR #4 TRANSVERSE BEAM HAS CRACK INDICATION AT OUTBOARD FLANGE. *** S/D *** R&R #4 TRANSVERSE BEAM IN AFT CARGO DOOR IAW FEDEX SRM 51-30-2.SDR 98FDEA00535Skin · creasedFWD CARGO DOOR OUTER SKIN IS DENTED 17 AFT OF FWD EDGE AND 27 UP FROM BOTTOM. *S/D* REPAIRED FWD CARGO DOOR 17 AFT OF FWD EDGE AND 27 UP FROM BOTTOM, PER FEDEX SRM 52-00-3.SDR 98FDEA00533Channel · crackedNR0424 FWD CARGO DOOR #4 TRANSVERSE BEAM (FROM BOTTOM) IS CRACKED IN OUTBOARD RADIUS. *** S/D ***R&R FWD CARGO DOOR #4 TRANSVERSE BEAM IAW FEDEX DRAWING 65-18620.SDR 98FDEA00532Shear Web · corrodedCORROSION (C53-224-08) ON SHEAR WEB BS 1166 TO 1174, LBL 37, WL 208. *S/D* REPAIRED SHEAR WEB AT BS 1166 TO 1174, LBL 37, WL 208 PER FED-EX SRM 51-40-2.SDR 98FDEA00516Skin · corrodedBS 440 TO 680, STR 1 TO STR 3 LT SHOWS SIGN OF CORROSION DUE TO SKIN PILLOWING AND DISHED RIVET HEADS. *S/D* REMOVED AND REPLACED CROWN SKIN AT STA 440 TO 740, STR 4 LT- STR 4 RT PER FED EX EA 7-5330-42276.SDR 98FDEA00485Longeron · corrodedSTA-PAE: CORROSION ON LONGITUDINAL BS 836 AND 839, RBL 45, WL 208.1. *S/D* REMOVED DAMAGE LONG BEAM FROM BS 760-850, RBL 45, WL 208.1 AND REPLACED PER FEDEX DRAWING 65-34144.SDR 98FDEA00470Skin · delaminatedNR 0455 005 STA-PAE: STEEL RUBSTRIP IS DISBONDED ON R/W I/B FOREFLAP I/B END. *** S/D *** REPAIRED R/W I/B FOREFLAP I/B END UPR & LWR SURFACES PER FEDEX SRM 51-40-6 & DRAWING 65-32738.SDR 98FDEA00469Fitting · crackedNR 0478 STA-PAE - VISUAL DAMAGE, CRACK AND CORROSION INDICATION NOTED IN HOLES NR 1 THROUGH 5 OF ROW 2 BS 870 RIGHT TERMINAL FITTING. REPAIRED HOLES NR 1 - 5 OF ROW 2, BS 870 RIGHT TERMINAL FITTING PER FEDEX EA 7-5310-39911.SDR 98FDEA00468Fitting · crackedNR 0421 STA-PAE - MECHANICAL DAMAGE NOTED IN HOLES NR 1 THROUGH 5 OF ROW 3 BS 870 LEFT TERMINAL FITTING. REPAIRED MECH DAMAGED HOLES IN LEFT TERMINAL FITTING AT BS 870 HOLE NR 1 THROUGH NR 5 OF ROW 3 PER EA NR 7-5310-39910.SDR 98FDEA00467Fitting · crackedNR0420 STA-PAE - CRACKS NOTED BY NDI IN HOLE NR 1 AND NR 2 OF ROW 2 BS 870 LEFT TERMINAL FITTING. REPAIRED LEFT TERMINAL FITTING AT BS 870 HOLE NR 1 AND NR 2 OF ROW 2 PER EA NR 7-5310-39910.SDR 98FDEA00466Fitting · crackedNR0479 STA-PAE - CRACK INDICATION NOTED IN HOLE NR 1 OF ROW 3, BS 870 RIGHT TERMINAL FITTING. REPAIRED HOLE NR 1 OF ROW 3, BS 870 RIGHT TERMINAL FITTING PER FEDEX EA 7-5310-39911.SDR 97FDEA00690Retract Mech · failedAFTER TAKEOFF, NR 2 LEADING EDGE FLAP WOULD NOT RETRACT WHEN HANDLE MOVED FROM 5 TO 2. RED TABS WHERE FOLLOWED BUT PROBLEM STILL EXIST RETURNED TO ATL. CLEANED AND RESEATED CANNON PLUG NR 2 LEADING EDGE FLAP, OPERATIONAL CHECK NORMAL.SDR 97FDEA00050Door Mechanism · not latchedAIRCRAFT WOULD NOT HOLD PRESSURE ABOVE 2,000 FT GROUND LEVEL. PRESSURIZATION WOULD RESPOND IN MANUAL BUT ONLY TO 10,000 CABIN PRESSURE. THEN EVEN IN FULL MANUAL INCREASE CABIN WOULD CLIMB AT 1,500 TO 1,800 FT PER MINIMUM RATE OF CLIMB. FORWARD ENTRY DOOR WASDR 96FDEA01055Hyd Line · leakingHYDRAULIC SYSTEM-A FAILURE, QTY DROPPED TO ZERO, MANUALLY CRANKED GEAR DOWN. FLUID SHUTOFF VALVES OFF FOR 30 MINUTES PRIOR TO ENGINE SHUTDOWN. PARTS CATALOG 27-60-00 FIG 20 PG 1, FOUND HYD FLUID LEAKING FROM B-NUT TO T-FITTING NR 60 AND A SMALLER LEAK AT T-FSDR 96FDEA00312Forging · crackedHFEC IND A CRACK IN LT STA 870 FORGING AT INTEGRAL RIB, BELOW CABIN FLOOR WL 190 ON TOP SIDE AT LOWER AFT FASTENER CRACK. ALSO, RUNNING UNDER RIB EXTENDING AFT. REMOVED INTEGRAL RIB FLUSH WITH WEB, PER ESO 11782. HFEC CONFIRMED NO CRACKS AFTER DAMAGE REMOVASDR 96FDEA00311Floorbeam · corrodedCABIN FLOORBEAM AT STA 950 IS CORRODED AROUND SCREW HOLES TOP AND BOTTOM OF BEAM FROM SEAT TRACK NR 3 TO NR 5. REMOVED CORROSION PER 51-10-06, OUT OF LIMITS. REPAIRED PER ESO 11782 AND FEDEX EA 7-5310-27477.SDR 96FDEA00310Bellframe · plugged holeSTR 27L BELLFRAME 990 PLUGGED HOLE TOP NEAR EXISTING FASTENER HOLE. INSTALLED DOUBLER PER SRM 51-40-3.SDR 96FDEA00309Web · corrodedLOWER FUSE CENTER TANK REAR SPAR UPPER CHORD, 3 RIVETS HAD POPPED 2 RIVETS WORKING, SKIN WARP BULGE LBL 18 TO 30. INSTALLED DOUBLER AND TRIPLER TO CENTER TANK UPPER WEB PER ESO 11782 DATED 2-13-96, AWAITING FEDEX EA.SDR 96FDEA00307Stringer · crackedUPPER LOBE MAIN CARGO INTERIOR STRUCTURE, STR 15L CRACKED AT FS 676. REMOVED DAMAGED SECTION OF STR 15L AND INSTALLED STR SPLICE REPAIR PER SRM 53-10-3 FIG 1 PG 3 TO 48.
Back to N118FE, cancelled Oct 31, 2002