N145FE, cancelled Oct 15, 2002

Service difficulty reports · 45

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 = 'N145FE' AND deregistration_id = 'N145FE-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 98FDEA00660Bulb · failedON APPROACH, WHEN GEAR HANDLE PUT DOWN BOTH LIGHTS IN RIGHT MAIN GEAR IND BURN OUT. DID GO-AROUND AND REPLACED BOTH BULBS, WORKED OK. CHECKED MAIN GEAR IND LIGHTS, CHECKS OK.Oct 21, 1998 · N145FE · Boeing 72727C · Landing Gear Position and WarningSDR 98FDEA00496Switch · malfunctioned98-0197 - NR 2 SLAT STILL IND OUT WHEN FLAP RETRACT TO ZERO POSITION TEST ALL AMBER LEADING EDGE SLATS ILLUM). AIRPLANE DID NOT HOWEVER ROLL LEFT. REQUIRES UNUSUAL CONTROL INPUTS TO KEEP WINGS LEVEL. FOUND NR 2 SLAT ACTUATOR POSITION SWITCH TO BE BAD. REPLAug 11, 1998 · N145FE · Boeing 72727C · Leading Edge Slat Position Indicating SystemSDR 98FDEA00327Indication · malfunctionedAFTER TAKEOFF WITH FLAPS SELECTED UP THE YELLOW LEADING EDGE FLAP INDICATOR STAYED ON WITH CORRESPONDING NR 7 SLAT INTRANSIT LIGHT ON THE SECOND OFFICERS'S AUXILIARY PANEL. CYCLED THE FLAP PER CHECKLIST, LIGHTS STAYED ON AS STATED ABOVE. RETURNED TO DEPARTUREMay 5, 1998 · N145FE · Boeing 72727C · Leading Edge Slat Position Indicating SystemSDR 98FDEA00143Stringer · corrodedNR 0776 036 CORROSION (C53-224-02) ON STRINGER 3 RT AT BS 540-740. REMOVED AND REPLACED STRINGER 3 RT FROM BS 520-620 AND FROM BS 650-740 IAW FED-EX SRM 53-10-03.Feb 28, 1998 · N145FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 98FDEA00083Stringer · crackedNR 0832 035, AFTER ACCESSING SKIN ON NR 0648, FOUND STRINGER 6 LT TO BE CRACKED AROUND A FASTENER HOLE AT BS 460. REMOVED AND REPLACED LT STRINGER NR 6 SECTION, BS 450-490 IAW FED-EX SRM 53-10-3.Feb 3, 1998 · N145FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00881Floorbeam · corrodedNR 0756 033 DOUBLE HOLES IN LOWER CHORD OF FLOORBEAM BS 540, LBL 19, WL 201. REMOVED DAMAGE AND REPAIRED IAW FED EA 7-5310-35019 AND 7017. REMOVED CORROSION FROM FLOORBEAM AT BS 540, LBL 19, WL 201. REPAIRED PER FED 7-5310-35019 AND 7017.Dec 5, 1997 · N145FE · Boeing 72727C · Fuselage Main, Floor BeamSDR 97FDEA00880Floorbeam · corrodedNR 0757 034 DOUBLE HOLES IN LOWER CHORD OF FLOORBEAM BS 600, LBL 19, WL 201. REMOVED DAMAGE AND REPAIRED IAW FED EA 7-5310-35019 AND 7017. REMOVED CORROSION FROM FLOORBEAM AT BS 600, LBL 19, WL 201. REPAIRED PER FED EA 7-5310-53019 AND 7017.Dec 5, 1997 · N145FE · Boeing 72727C · Fuselage Main, Floor BeamSDR 97FDEA00878Strap · corrodedCORROSION (C53-132-01) WHILE WORKING NR0732 DISCOVERED CORROSION ON LOWER SURFACE OF MAIN FRAME STRAP BS 950, RBL 30, WL 144. *S/D* REMOVED CORROSION ON LOWER MAIN FRAME STRAP AT BS 950, RBL 30, WL 144 AND BS 950, STR 24R TO STR 27R. FABRICATED REPAIR PARTSDec 4, 1997 · N145FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00858Floorbeam · corrodedCORROSION (C53-224-02) EMANATING FROM UNDER NUT PLATE BS 600 FLOORBEAM UPPER CHORD RBL 45 TO 60, WL 208. *S/D* REPAIRED FLOORBEAM AT BS 600, RBL 45 TO 60, WL 208 PER FEDEX SRM 53-10-8.Nov 24, 1997 · N145FE · Boeing 72727C · Fuselage Main, Floor BeamSDR 97FDEA00853Skin · corrodedCORROSION (C53-224-02) ON INNER SKIN BS 680, STR 12 TO 13 RT. *S/D* REPAIRED INNER SKIN AT BS 680, STR 12 TO 13 RT PER FEDEX EA 7-5330-36188.Nov 21, 1997 · N145FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 97FDEA00852Floorbeam · corrodedCORROSION (C53-111-01,3) ON LOWER CHORD OF FLOORBEAM AT BS 1050 FROM RBL 47 TO LBL 47, WL 200. *S/D* REMOVED AND REPLACED FLOORBEAM LOWER CHORD BS 1050, RBL 70 TO LBL 70, WL 200 IAW FEDEX EA 7-5310-34970A.Nov 21, 1997 · N145FE · Boeing 72727C · Fuselage Main, Floor BeamSDR 97FDEA00657Skin · crackedCRACKED SHEAR T/E BS 1282 BETWEEN STR 17 TO 18 RT. *S/D* REMOVED CRACKED SHEAR T/E BS 128.2, STR 17 TO 18 RT. FOUND EXTERNAL SKIN TO BE DAMAGED. REPAIRED EXTERNAL SKIN BS 1271 TO 1287, STR 17 TO 19 RT IAW FED-EX SRM 53-30-3. FABRICATED NEW SHEAR T/E, INSTSep 16, 1997 · N145FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 97FDEA00580Stringer · crackedWHILE WORKING NR 0271, FOUND STRINGER 15 RT CRACKED AT BS 1282. *S/D* REMOVED DAMAGED SECTION OF STRINGER, FABRICATED AND INSTALLED REPAIR FROM BS 1279 TO 1289 IAW FED-EX SRM 53-10-3.Aug 25, 1997 · N145FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00574Stringer · corrodedCORROSION (C53-224-01,1) ON STRINGER 8 RT, BS 480 TO 600. *S/D* REPAIRED STR 8 RT, BS 480 TO 490 PER FED-EX SRM 53-10-3.Aug 25, 1997 · N145FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00527Stringer · crackedAFTER ACCESSING SKIN ON NR 0648, FOUND STRINGER TO BE CRACKED AT BS 460, STRINGER 8 LT. *S/D* REMOVED DAMAGED SEGMENT OF STR 8 LT, BS 450 TO 490 IAW FED-EX SRM 53-10-3. FABRICATED SEGMENT OF STR 8 LT, BS 450 TO 490 AND PLATES IAW FED-EX SRM 53-10-3. ALODINAug 12, 1997 · N145FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00524Stringer · crackedWHILE WORKING NR 0832, FOUND LT STRINGER 9 TO BE CRACKED AROUND FASTENER HOLES AT BS 460. *S/D* REPAIRED CRACKS AROUND FASTENER HOLES AT BS 460, STR 9L PER FED SRM 53-10-3.2.Aug 11, 1997 · N145FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00523Terminal Fitting · corrodedWHILE WORKING NR 0696, FOUND CORROSION THE AFT EDGE OF L/W AFT TERMINAL FITTING. *S/D* REMOVED BOTTLE PIN AND BUSHING, REAMED FITTING, INSTALLED NEW BUSHING AND BOTTLE PIN AFTER CORROSION REMOVED IAW FED-EX SRM 51-10-1, FED-EX M/M 57-41-11.Aug 11, 1997 · N145FE · Boeing 72727C · Wing, Fuselage Attach FittingsSDR 97FDEA00517Stringer · corrodedWHILE WORKING NR 0832 FOUND CORROSION ON LT NR 7 STRINGER AT BS 463. *S/D* STRINGER 7 LT WAS REPLACED AT BS 454 TO 466 IAW FED-EX SRM 53-10-3.Aug 9, 1997 · N145FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00516Stringer · corrodedNR 0485 022 CORROSION (C53-224-01(3)) ON STRINGER 2 LEFT, BS 950-1110.Aug 9, 1997 · N145FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00519Frame · crackedNR 0711 020 CORROSION (C53-111-01-2) AROUND FASTENER HEAD IN AFT CARGO DOOR FRAME AT FLOOR BS 576, RBL 25, WL 155.Aug 7, 1997 · N145FE · Boeing 72727C · Fuselage Main, FrameSDR 97FDEA00514Skin · corrodedWHILE WORKING NR 0648 FOUND CORROSION (C53-224-02) UNDER LAP AT FRAME LOCATIONS FROM 640 TO 720 STRINGER 4 RT. *S/D* REPAIRED LOWER SKIN AT STR 4R, BS 460 TO 480 AND LOWER SKIN AT STR 4R, BS 480 TO 740 WAS REPAIRED ON NR 0648 IAW FED-EX EA NR 7-5310-32037.Aug 7, 1997 · N145FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 97FDEA00501Frame · crackedNR 0799 016 CRACK IN BS 277 FRAME AT STR 4R ATTACH POINT. REMOVED DAMAGED AREA AND REPAIRED FRAME AT BS 277 AT STR 4R ATTACH POINT PER FED SRM 51-40-3.Aug 5, 1997 · N145FE · Boeing 72727C · Fuselage Main, FrameSDR 97FDEA00500Stringer · corrodedCORROSION (C53-224-01,3) ON STRINGER 3 RT BS 950 TO 1183. *S/D* REMOVED CORROSION ON STR 3 RT, BS 950 TO 1183. REMOVED 2 SECTION OF STR 3 RT AT BS 1015 TO 1017. REPLACED 2 SECTION OF STR 3 RT AT BS 1015 TO 1017 IAW FED-EX SRM 53-10-3.Aug 4, 1997 · N145FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00499Stringer · corrodedCORROSION (C53-224-02) ON STRINGER 8 LT, BS 360 TO 480. *S/D* REPAIRED DAMAGED SECTION OF STR 8 LT, BS 371 TO 373 IAW FED-EX SRM 53-10-3.Aug 4, 1997 · N145FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00498Skin · corrodedNR 0805 CORROSION (C53-224-01(1)) ON INNER SKIN BS 783 - 804, STR 4 TO 6 RT. REMOVED CORROSION AND REPAIRED INNER SKIN BS 783-804, STR 4 TO 6 RT IAW FED-EX SRM 53-30-3. CORROSION FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-30-1.Aug 4, 1997 · N145FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 97FDEA00497Skin · corrodedCORROSION (C53-224-02) ON INNER SKIN, BEAR STRAP AND EMANATING FROM UNDER BEAR STRAP BS 460 TO 640, BETWEEN STRINGERS 2 LT AND 3 LT. *S/D* ACCOMPLISHED CROWN SKIN REPAIR BS 440 TO 740, STR 4R TO 10L PER FED-EX EA NR 7-5310-32037 AND 7-5100-37444.Aug 4, 1997 · N145FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 97FDEA00496Former · corrodedCORROSION (C53-132-01) BS 960 SKIN FORMER RBL 28, WL 144. * S/D* REMOVED CORRODED SKIN FORMER AT BS 960, RBL 28, WL 144. REPLACED WITH NEW SKIN FORMER. ALL WORK DONE PER FED SRM 53-10-1 AND 51-30-2.Aug 1, 1997 · N145FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00493Chord · corrodedCORROSION (C53-111-01-,2) ON BL 0 CHORD AROUND NUT PLATE HOLES ON O/B FLANGES FROM BS 490 TO 670, LBL 2- RBL 2, WL 20, OUT OF LIMITS PER FED-EX SRM. *S/D* REMOVED DAMAGED CHORD, FABRICATED NEW CHORD AND INSTALLED AT BS 480 TO 700 IAW FED-EX SR-27-53-009.Jul 31, 1997 · N145FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00491Stringer · corrodedCORROSION (C53-224-012) ON STR 4 LT, BS 804 TO 870. *S/D* REPAIRED DAMAGED AREA OF STR 4 LT, BS 845 IAW FED-EX SRM 53-10-3.Jul 30, 1997 · N145FE · Boeing 72727 · Fuselage Main, Longeron/StringerSDR 97FDEA00486Stringer · corrodedCORROSION (C53-224-02) ON STRINGER 4 RT, BS 660 TO 740. *S/D* REPAIRED STRINGER 4 RT, BS 650 TO 740 IAW FED-EX SRM 53-10-03.Jul 30, 1997 · N145FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00485Floorbeam · corrodedCORROSION (C53-224-01,1) ON BS 480 FLOORBEAM UNDERSIDE OF TOP CHORD LBL 45 TO 65, WL 208. *S/D* REMOVED CORROSION BETWEEN BL 0 AND RBL 20 ON TOP OF BS 480 FLOORBEAM. REMOVED CORROSION IN A 6 X 2 AREA. REMOVED .045 OF MATERIAL FROM ORIGINAL THICKNESS OF .22Jul 29, 1997 · N145FE · Boeing 72727C · Fuselage Main, Floor BeamSDR 97FDEA00474Stringer · corrodedNR 0491 007 CORROSION (C53-224-01(2)) ON STR 5 RT, BS 740 - 870. MECHANICALLY REMOVED CORROSION FROM STR 5 RT, BS 740-870. REMOVED UP TO .006 OF MATERIAL IN A 1 BY 36 AREA. ORIGINAL THICKNESS IS .056, FOUND TO BE OUT OF LIMITS PER FED SRM 53-10-1 FROM BS 74Jul 28, 1997 · N145FE · Boeing 72727C · Fuselage Main, Longeron/StringerSDR 97FDEA00475Floorbeam · corrodedCORROSION AROUND FASTENER HOLES BOTTOM SIDE BS 560 FLOORBEAM, UPPER CHORD RBL 47 TO 60 WL 208. *S/D* CORROSION BEYOND LIMITS, REMOVED, FABRICATED, INSTALLED UPPER T-CHORD AT BS 560 WL 208, RBL 47 TO 60 IAW FED-EX SRM 53-10-8.Jul 26, 1997 · N145FE · Boeing 72727C · Fuselage Main, Floor BeamSDR 97FDEA00473Strap · corrodedCORROSION (C53-111-01, 3) ON CENTRAL STABILIZER STRAP AT NUT PLATES FROM BS 1028 TO BS 1110, RBL 2 TO LBL 2, WL 200. *S/D* REMOVED DAMAGED STRAP, CENTER STABILIZER, BS 1028 TO 1110, RBL 2 TO LBL 2, WL 200. FABRICATED AND INSTALLED NEW ONE IAW SR-27-53-009.Jul 25, 1997 · N145FE · Boeing 727227 · Fuselage Miscellaneous StructureSDR 97FDEA00468Floorbeam · corrodedCORROSION (C53-224-04) AROUND FASTENER HOLES ON BS 1030 FLOORBEAM UPPER CHORD LBL 47 TO 60, RBL 47 TO 60, WL 208. *S/D* REMOVED UPPER FLOORBEAM CHORD AND REPLACED IN (2) TWO PLACES RBL 14.5 TO SKIN BS 1030, WL 208 IAW FED SRM 53-10-8.Jul 23, 1997 · N145FE · Boeing 72727C · Fuselage Main, Floor BeamSDR 97FDEA00467Floorbeam · corrodedCORROSION (C53-224-04) ON BS 1110 FLOORBEAM UPPER CHORD AROUND FASTENER HOLES RBL 47 TO 60, WL 208. *S/D* REMOVED UPPER FLOORBEAM CHORD AND REPLACED AT RBL 17 TO SIDEWALL, WL 208, BS 1110, IAW FEDEX SRM 53-10-8.Jul 23, 1997 · N145FE · Boeing 72727C · Fuselage Main, Floor BeamSDR 97FDEA00466Web · corrodedCORROSION (C53-221-01) UNDERSIDE OF HORIZONTAL WEB BS 228 TO 238, RBL 45, WL 232. *S/D* CORROSION ON WEB FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. FABRICATED NEW AND REPLACED OLD WEB PER DRG 5-71775 AND FED-EX SRM 51-30-2.Jul 22, 1997 · N145FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 97FDEA00465Floorbeam · corrodedNR 0747 002 CORROSION (C53-111-01-2) AROUND NUTPLATE ON MAIN FLOORBEAM BS 560, LBL 58, WL 208. REMOVED CORROSION ON FLOORBEAM AT BS 560, LBL 58 AND INSTALLED BEAM REPAIR PER FED-EX SRM 53-10-8, 53-10-1, 51-20-1, 51-40-2.Jul 22, 1997 · N145FE · Boeing 72727C · Fuselage Main, Floor BeamSDR 97FDEA00455Floorbeam · corrodedNR 0635 001 CORROSION ON BS 950 FLOORBEAM UPPER CHORD AT LBL 20, LBL 47 - 55, RBL 52 - 54, WL 208. CORROSION ON BS 950 FLOORBEAM UPPER CHORD AT LBL 20, LBL 47 - 55, RBL 52 - 54, WL 208.Jul 21, 1997 · N145FE · Boeing 72727C · Fuselage Main, Floor BeamSDR 96FDEA01414Acm · oil leakSMOKE IN CARGO COMPARTMENT. NOT RECOGNIZABLE ODOR. REQUIRED USE OF OXYGEN MASKS AND EMERGENCY DESCENT. FOUND OLD ACM LEAKING OIL AND BYPASSING INTERNALLY CAUSING SMOKE IN CARGO COMPARTMENT. REMOVED AND REPLACED RIGHT HAND A.C.M. PER MM 21-51 AS REQUIRED. Aug 27, 1996 · N145FE · Boeing 72727 · Cabin Cooling SystemSDR 95FDEA01912Actuator · malfunctionedWHEN RETRACTING FLAPS TO A 2 DEGREE POSITION AFTER TAKEOFF, NR 5 LED REMAINED EXTENDED, FLAPS POSITIONED TO 5 DEGREES NORMAL LED EXTENSION, FLAPS TO 2 DEGREE POSITION REMAINED EXTENDED. REMOVED AND REPLACED NR 5 L/E FLAP ACTUATOR. OPS AND LEAK CHECKS NORMAL Dec 21, 1995 · N145FE · Boeing 72727C · Leading Edge Slat ActuatorSDR 95FDEA00193Vertcal Beam · misdrilledWHILE WORKING EO 7-5310-7-23550 FOUND EXTRA HOLE DRILLED IN VERTICAL BEAM AT RBL 46 WL 243 BS 1178. BLENDED DAMAGE AT RBL 46 WL 243 BS 1178. SUBMIT TO ENGINEERING FABRICATED REPAIR PARTS IAW FEDEX SRM 51-40-4 AND 53-10-2. INSTALLED WET WITH SEALANT AND INSTFeb 28, 1995 · N145FE · Boeing 72727C · Fuselage Miscellaneous StructureSDR 95FDEA00186Skin · corrodedSKIN BULGE AND RIVETS HEADS POPPING AT SKIN LAP BS 1280, STR 10L. REPAIRED SKIN LAP STA 1280, STR 19L PER FEDEX SRM 53-30-3.Feb 25, 1995 · N145FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 95FDEA00185Skin · gougedGOUGE IN SKIN BS 1280 JUST ABOUT STR 21R .020 D OUT OF LIMITS PER SRM. REPAIRED PER FEDEX SRM 53-30-2.Feb 25, 1995 · N145FE · Boeing 72727C · Fuselage Main, Plate/SkinSDR 95FDEA00172Clip · crackedCORROSION IN AFT CARGO BAY THERE IS CORROSION ON STR CLIP AT BS 970, STR 30. REMOVED AND FABRICATED STR CLIP 7076T6-050 AND INSTALLED STR CLIP.Feb 22, 1995 · N145FE · Boeing 72727C · Fuselage Miscellaneous Structure
Back to N145FE, cancelled Oct 15, 2002