N146FE, cancelled Oct 15, 2002

Service difficulty reports · 74

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 = 'N146FE' AND deregistration_id = 'N146FE-2002-10-15'
  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.

SDR 01FDEA00383Valve · stuckNR 3 FUEL CROSSFEED VALVE W/N OPEN. *S/D* REMOVED AND REPLACED CROSSFEED VALVE ACTUATOR PER MM 28-22-011-4 PAR 4 A-D & PAR 9 A-P. VALVE OPS CK GOOD.May 24, 2001 · N146FE · Boeing 72727C · Fuel Transfer ValveSDR 01FDEA00350Outflow Valve · failedA/C WILL NOT PRESSURIZE, EITHER PACK ANY BLEED SOURCE, MANUAL OR AUTO MODE. NO DOOR LIGHTS ILLUM ON 2ND OFF PNL. R&R LT & RT OUTFLOW VALVE & CABIN PRESSURE CONTROLLER PER 727 MM 21-30-051-4, 21-31-010-4 & 21-30-000-5.May 15, 2001 · N146FE · Boeing 72727C · Pressure Regulator/Outflow ValveSDR 00FDEA00437Bracket · separatedDURING A ROUTINE INSP, FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE LIGHT BRACKET WAS FND SEPARATED FROM LIGHT. REPAIRED BRACKET ASSY PER IAW SRM 51-30-2.Jul 6, 2000 · N146FE · Boeing 72727C · Passenger/Crew DoorsSDR 00FDEA00436Splice · corrodedDURING ROUTINE INSP, THE CENTER WING AFT UPPER SPAR SPLICE AT BS 870, RBL 70.5 FND CORRODED BEYOND ALLOWED LIMITS. R&R PER IAW SRM 51-30-2.Jul 6, 2000 · N146FE · Boeing 72727C · Wing, Center BoxSDR 00FDEA00432Spoiler · crackedDURING ROUTINE INSPECTION NR 10 SPOILER SKIN FOUND CRACKED AT CENTER MOUNTING LUG. R&R IAW MM 27-61-001-4. RIGGED & OPS CHECKED SPOILER IAW MM 27-61-001-5.Jul 5, 2000 · N146FE · Boeing 72727C · SpoilersSDR 00FDEA00431Fitting · crackedN 349 DURING ROUTINE INSPECTION, BS 870 RT, TERMINAL FITTING FOUND CRACKED AT FWD UPPER FASTENER HOLE AT S-9 RT. R&R PER IAW FEDEX EA 7-5310-50105.Jul 5, 2000 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 00FDEA00430Spoiler · crackedDURING ROUTINE INSPECTION, NR 11 SPOILER PANEL WAS FOUND CRACKED. R&R IAW SRM 51-40-6. RIGGED & OPS CHECK SPOILER IAW MM 27-61-001-5.Jul 5, 2000 · N146FE · Boeing 72727C · SpoilersSDR 00FDEA00429Skin · corrodedN 165 DURING ROUTINE INSPECTION, FUSELAGE SKIN WAS FOUND BULGED BETWEEN STR 24 LT & 27 LT JUST AFT OF BS 1183. R&R IAW SRM 53-30-3.Jul 5, 2000 · N146FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 00FDEA00428Skin · crackedDURING ROUTINE INSPECTION, FUSELAGE SKIN WAS FOUND CRACKED AT STR 1, BS 430. R&R PER IAW SRM 53-30-3 FIG 4.Jul 5, 2000 · N146FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 00FDEA00427Skin · corrodedDURING ROUTINE INSPECTION, CORROSION FOUND ON EXTERNAL FUSELAGE BETWEEN STR 7 RT TO 10 RT FROM BS 1173 - 1183. R&R SKIN BETWEEN STR 3 RT & 10 RT FROM BS 1080 - 1183 IAW BOEING DRAWING 65-18382 & SRM 51-30-2.Jul 5, 2000 · N146FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 00FDEA00426Slide · tornN 45 DURING ROUTINE INSPECTION, FWD ENTRY DOOR EMERGENCY ESCAPE SLIDE GIRT ASSY FOUND FRAYED & TORN. R&R GIRT ASSY IAW SRM 51-40-9.Jul 5, 2000 · N146FE · Boeing 72727C · Escape SlideSDR 99FDEA00278Switch · sticksAFT CARGO DOOR LIGHT ILLUMINATED AFT T/O, LIGHT EXT ON APPROACH, AT APPROACH SPD. FOUND INNER DOOR SWITCH STUCK. LUBED SWITCH, OPS CK NORMAL.Jul 23, 1999 · N146FE · Boeing 72727C · Door Warning SystemSDR 98FDEA00023Battery · dischargedFORWARD ENTRY DOOR ESCAPE SLIDE EMERGENCY LIGHT BATTERY IS DEAD. *S/D* REMOVED AND REPLACED FWD ENTRY DOOR ESCAPE SLIDE EMERGENCY LIGHT BATTERY AND FUNCTIONAL TESTED IAW FED-EX M/M 33-50-121.Jan 12, 1998 · N146FE · Boeing 72727C · Emergency LightingSDR 97FDEA00908Bracket · corrodedNR 0179 058 - R/W I/B AILERON, TURNAROUND CASTING CORRODED.Dec 31, 1997 · N146FE · Boeing 72727C · Wing Miscellaneous StructureSDR 97FDEA00903Spar Chord · corrodedNR 0251 057 CORROSION (C57-581-04-01) L/W T/E UPPER CHORD ABOVE NR 1 FLAP TRANSMISSION. REPAIRED L/W T/E UPPER SPAR CHORD ABOVE NR 1 FLAP TRANSMISSION IAW FED-EX EA NR 7-5710-36849.Dec 29, 1997 · N146FE · Boeing 72727C · Wing SparSDR 97FDEA00902Fitting · corrodedNR 0622 056 CORROSION (C57-581-01) L/W O/B AILERON LOCKOUT FILLING IS CORRODED, AREA MARK. REMOVED AND REPLACED AILERON LOCKOUT FITTING IAW FED-EX EA NR 7-5710-37352.Dec 29, 1997 · N146FE · Boeing 72727C · AileronsSDR 97FDEA00896Stringer · corrodedNR 0186 055 CORROSION (C53-224-01) ON STRINGER 2 LT, BS 950-1183. REPAIRED STR 2 LT, BS 950-1183 IAW FEDEX SRM 53-10-3.Dec 21, 1997 · N146FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00895Stringer · corrodedNR 0646 053 CORROSION (C53-224-01) ON STR 5 LT, BS 970 - 990. REPAIRED STR 5 LT, BS 950-998 IAW FED-EX SRM 53-10-3.Dec 19, 1997 · N146FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00894Spar · corrodedNR 0970 054 CORROSION ON VERTICAL STABILIZER INTER SPAR SKIN BS 1340 - 1344, LBL 18, WL 260.Dec 19, 1997 · N146FE · Boeing 72727C · Vertical Stabilizer, Spar/RibSDR 97FDEA00891Fitting · crackedWHILE WORKING NR0842, DISCOVERED CRACK IN FORWARD I/B RADIUS OF LT 870 TERMINAL FITTING, 2.8 INCHES ABOVE STR 10 TO 1.7 INCHES BELOW STR 10.Dec 17, 1997 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00889Skin · dentedNR 0939 050 WHILE WORKING NR0829 DISCOVERED DENT IN EXTERIOR SKIN BS 380, STR 21L. REMOVED DENTED AREA AT BS 380, STR 21L PER FED-EX SRM 53-20-3. FABRICATED PATCH AND INSTALLED PER FED-EX SRM 53-30-3, SRM FED-EX SRM 51-10-2.Dec 15, 1997 · N146FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 97FDEA00888Clips · gougedNR 0648 051 DAMAGED STRINGER CLIPS BS 970, STR 7 LT, BS 990, STR 7, RT, BS 1010, STR 5 RT AND 5 LT. REPLACED STR CLIPS AT BS 970, STR 7L, BS 990, STR 7R, BS 1010, STR 5R AND BS 1010, STR 5L, IAW FEDEX SRM 51-30-2.Dec 15, 1997 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00887Floorbeam · corrodedNR 0937 049 CORROSION (C53-224-01) ON FLOORBEAM BS 1130, RBL 16 - RBL 31, WL 208. REMOVED UPPER CHORD OF FLOORBEAM AT BS 1130, RBL 15 TO RBL 39, WL 208 AND REPAIRED IAW FED-EX EA NR 7-5310-37355 AND ER 97-2706.Dec 13, 1997 · N146FE · Boeing 72727C · Fuselage Main, Floor BeamSDR 97FDEA00871Strap · corrodedCORROSION (C53-111-01, 2) ON I/B STRAP BS 500 TO 600, RBL 25, WL 156 FWD CARGO BAY. *S/D* REMOVED AND REPLACED I/B STRAP BS 500 TO 600, RBL 25, WL 156 FWD CARGO BAY PER FED SRM 51-30-02.Dec 1, 1997 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00870Chord · corrodedCORROSION (C53-111-01, 2) UNDER NUT PLATES ON BL 0 CHORD BS 450 TO BS 680, WL 200. FWD CARGO BAY AS PER FEDEX DRAWING SR 27-53-009 AND FASTENER INSTALLATION AS PER FEDEX SRM 51-30-02. *S/D* REMOVED AND REPLACED BL 0 CHORD FROM BS 450 TO BS 740, WL 200 IN FWDec 1, 1997 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00865Skin · corrodedNR 0673 045 CORROSION (C53-224-01) ON INSIDE SKIN BETWEEN BS 710-660 AND STR 4 RT, 6 LT CROWN AREA (MARKED IN RED). CUT OUT DAMAGED AREAS AND REPAIRED SKIN BETWEEN BS 660-710, STR 4 RT, STR 6 LT IAW FED-EX SRM 53-30-3.Nov 25, 1997 · N146FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 97FDEA00864Fitting · corrodedNR 0950 046 CORROSION (C53-224-01(2)) BARRIER NET CASTING BS 360, RBL 20. REMOVED AND REPLACED BARRIER NET CASTING BS 360, RBL 20 PER FED-EX SRM 51-30-2.Nov 25, 1997 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00861Fitting · crackedNR 0842 044 CRACK INDICATION NOTED LT 870 TERMINAL FITTING ROW 3, HOLE NR 3. REPAIRED LT BS 870 TERMINAL FITTING AS PER FED-EX EA NR7-5310-37383.Nov 24, 1997 · N146FE · Boeing 72727C · Fuselage, Wing Attach FittingsSDR 97FDEA00860Floorbeam · corrodedCORROSION AFT BAY BS 1130 LOWER FLOORBEAM CHORD LOWER SURFACE LBL 21, WL 200 AT FASTENER HOLE. *S/D* REPAIRED AFT BAY BS 1130 LOWER BEAM CHORD, LOWER SURFACE, LBL 21, WL 200 PER ER 97-2664 AND EA 7-5310-36853.Nov 24, 1997 · N146FE · Boeing 72727C · Fuselage Main, Floor BeamSDR 97FDEA00859Fitting · crackedCRACK INDICATION NOTED IN RT BS 870 TERMINAL FITTING ROW 3, HOLE NR 2. *S/D* REPAIRED CRACKED FASTENER HOLE IN THE 870 RT TERMINAL FITTING ROW 3, HOLE NR 2 IAW FEDEX EA NR 7-5310-37308.Nov 24, 1997 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00855Beam · corrodedNR 0459 041 CORROSION (C53-224-01(2) BS 950 UPPER CHORD BL-O-LBL 24, RBL 45-62. UPPER SURFACE AND RBL 62-LBL 46 ON LOWER SURFACE AT NUTPLATES. ACCOMPLISHED REPAIR ON BS 950 BEAM IAW FED EA NR 7-5310-36830.Nov 24, 1997 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00848Floorbeam · corrodedCORROSION (C53-111-01, 3) AFT BAY BS 1148, RBL 35 - BL 0, WL 208 AT FASTENER HOLES. *S/D* REPAIRED FLOORBEAM AT BS 1148 LOWER CHORD, RBL 35 TO BL 0, WL 208 IAW FED-EX SRM 53-10-8.Nov 20, 1997 · N146FE · Boeing 72727C · Fuselage Main, Floor BeamSDR 97FDEA00847Spar Web · corrodedNR 0952 039 CORROSION (C53-395-11) ON VERTICAL STABILIZER INTER SPAR SKIN BS 1340 - 1344, RBL 18, WL 260. REPAIRED CORROSION ON RT INNER SPAR SKIN OF VERT STAB BS 1340-1344, RBL 18, WL 260 IAW FED-EX EA NR 75510-37338 AND FED-EX EA NR 7-5330-37334.Nov 20, 1997 · N146FE · Boeing 72727C · Vertical Stabilizer, Spar/RibSDR 97FDEA00846Spar Chord · corrodedNR 0949 038 WHILE WORKING (FEDEX CARD NR 0652) FOUND LT REAR VERTICAL SPAR CORRODED AT BS 1342. REMOVED AND REPLACED SECTION OF THE LT VERTICAL SPAR CHORD BS 1342, FIN STA 0.00 TO FIN STA 99.0 IAW FED-EX EA NR 7-5530-37380.Nov 20, 1997 · N146FE · Boeing 72727C · Vertical Stabilizer, Spar/RibSDR 97FDEA00845Spar · corrodedNR 0948 037 WHILE WORKING (FEDEX CARD NR 0652) FOUND RT REAR VERTICAL SPAR CORRODED AT BS 1342. REPLACED RT REAR VERTICAL SPAR CHORD FROM BS 1342 TO FIN STA 55, RBL 18 IAW FED-EX EA NR 7-5510-37337.Nov 20, 1997 · N146FE · Boeing 72727C · Rudder, Spar/RibSDR 97FDEA00844Stringer · corrodedCORROSION (C53-224-01) ON STRINGER 2 RT, BS 700 TO 640 (MARKED). *S/D* REMOVED CORROSION ON STR 2 RT, BS 700 TO 640. FOUND AREA 1.25 X .375 AT BS 697 TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1. FABRICATED AND INSTALLED REPAIR IAW EA NR 7-5310-36831.Nov 19, 1997 · N146FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00840Skin · corrodedUPON REMOVAL OF UPPER CHORD (NR0413) FOUND INSIDE UPPER TANK SKIN TO BE CORRODED, BS 870, RBL 60 - LBL 60, WL 178. *S/D* REMOVED CORROSION INSIDE UPPER TANK SKIN BS 870, RBL 60 - LBL 60, WL 178 PER FED EA 7-5710-36884 AND ER 97-3658.Nov 17, 1997 · N146FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 97FDEA00839Skin · corrodedUPON REMOVAL OF LOWER CHORD (NR0145) FOUND INSIDE LOWER TANK SKIN TO BE CORRODED BS 870, RBL 60- LBL 60, WL 148. *S/D* REMOVED CORROSION ON INSIDE LOWER TANK SKIN BS 870, RBL 60 - LBL 60, WL 148 PER FED 53-10-1 AND EA 7-5710-36884 AND ER 97-2658.Nov 17, 1997 · N146FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 97FDEA00838Bulkhead Strap · corrodedUPON REMOVAL OF 8.70 BULKHEAD WEB (NR0414) FOUND TENSION LOAD STRAP TO BE CORRODED RBL 50-LBL 50, WL 160. *S/D* REMOVED AND REPLACED TENSION LOAD STRAP RBL 65 - LBL 65, WL 160, BS 870 PER BOEING DWG 65-15978 AND ER NR 054. INSTALLED HILOCS PER FED SRM 51-30Nov 14, 1997 · N146FE · Boeing 72727C · Fuselage Main, BulkheadSDR 97FDEA00837Chord · corrodedCORROSION (C53-224-01, 2) AND BORE METAL ON LONGITUDINAL BS 760 TO 848, WL 208, RBL 48 ON LOWER SURFACE OF INBOARD FLANGE AT NUTCLIP LOCATIONS.Nov 14, 1997 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00836Chord · corrodedCORROSION (C53-224-01,2) LONGITUDINAL BS 760 TO 848, WL 208 UPPER AND LOWER FLANGE SURFACES AT NUTCLIP LOCATIONS. *S/D* REMOVED AND REPLACED LONGITUDINAL BS 760 TO 848, WL 208, RBL 24 UPPER CHORD IAW FED DWG 65-34144.Nov 14, 1997 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00835Chord · corrodedCORROSION (C53-224-01, 2) LONGITUDINAL BS 760 TO 848, WL 208, LBL 45 AT NUTCLIP LOCATIONS ON UNDERSIDE OF FLANGE BS 820 ON UPPER SURFACE AND SEAT TRACK FASTENER CUTOUT BS 760.Nov 14, 1997 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00823Stringer · crackedCRACK IN STRINGER 24 RIGHT UNDER 1010 FRAME. *S/D* STOP DRILLED CRACK PER FED-EX SRM 51-10-1, FABRICATED J-CHANNEL PER FED-EX SRM 53-10-3. ALODINED AND PRIMED PER FED-EX SRM/ MM 51-10-2 AND 51-20-151. INSTALLED J-CHANNEL REPAIR PER FED-EX SRM 53-10-3.Nov 11, 1997 · N146FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00822Skin · corrodedCORROSION ON FORWARD SIDE OF BS 481 SPLICE PLATE BETWEEN STRINGER 5 RT AND 6 RT.Nov 11, 1997 · N146FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 97FDEA00816Stringer · corrodedCORROSION (C53-224-01) ON STRINGER 3 LT, BS 445 TO 360 IN AREAS (MARKED IN RED). *S/D* REPAIRED STR 3 LT, BS 377 TO 387, BS 417 TO 428 PER FED-EX EA 7-5310-36840.Nov 10, 1997 · N146FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00815Fitting · corrodedCORROSION (C53-111-01-1) STR 26R FITTING BS 360. *S/D* REMOVED CORROSION ON SHEAR TIE FITTING BS 360, STR 26R PER FED SRM 53-10-1. INSTALLED NEW SHEAR TIE FITTING BS 360, STR 26R PER FED SRM 51-30-2 PG 2B.Nov 10, 1997 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00814Stringer · corrodedCORROSION (C53-224-01) ON STRINGER 2 LT, BS 360 TO 430 (AREA MARKED IN RED). *S/D* REPAIRED STR 2 LT, BS 360 TO 430 IAW FED-EX SRM 53-10-3.Nov 10, 1997 · N146FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00803Strap · corrodedCORROSION BS 475 BETWEEN STRINGER 2 AND STRINGER 3 LT. *S/D* REPAIRED CORROSION AT BS 475 BETWEEN STR 2 AND STR 3 LT IAW FED EA NR 7-5330-37314.Nov 3, 1997 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00802Strap · corrodedCORROSION (C53-224-01, 1) EMANATING UNDER STRINGER ON MCD BARE STRAP FROM BS 460 TO 480 STRINGER 3 LT.Nov 3, 1997 · N146FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00797Skin · corrodedNR 0645 022 CORROSION (C53-224-01) ON INTERNAL SKIN 950-990 STR 1 - STR 4 RT. REPAIRED SKIN BS 950-990, STR 1 - STR 4 RT IAW FED-EX SRM 53-30-3 FIG 3.Oct 31, 1997 · N146FE · Boeing 72727C · Fuselage Main, Plate/Skin
Back to N146FE, cancelled Oct 15, 2002