N144FE, cancelled Aug 26, 2004

Service difficulty reports · 61

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 = 'N144FE' AND deregistration_id = 'N144FE-2004-08-26'
  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 02FDEA00315Wire · damagedDURING TAXI ELEVATOR FEEL DIFFERENTIAL LIGHT CAME ON. LOW PRESS LIGHT C/B ON. HYD A & B FILTERS CHECK GOOD. PITOT TUBES ON TAIL WERE CLEAN. SPLICED IN NEW SECTION OF WIRE PER SMP, OPS CHECK NORMAL.May 7, 2002 · N144FE · Boeing 72721C · Flight Control System WiringSDR 00FDEA00391Door · not closedAIRFRAME VIBRATION AND HUMMING SOUND. INSP GROUND PWR SERVICE DOOR. NO DEFECTS NOTED. RESECURED DOOR CLOSED.Jun 16, 2000 · N144FE · Boeing 72721C · Service DoorsSDR 00FDEA00273Handle · wornON FINAL APPROACH, GEAR HANDLE DOWN, HEARD NOISE. FELT MUSHY. NOSE GEAR AND NOSE DOORS UNSAFE RED LIGHT ON RECYCLED GOT GOOD IND ON ALL 3 GEAR. LANDING GEAR CONTROL HANDLE CABLE TENSION LOW. ADJUSTED PER MM 32-31-000-5 PG 501-505. REMOVED AND REPLACED SELApr 19, 2000 · N144FE · Boeing 72721C · Landing Gear SelectorSDR 99FDEA00268Warning Switch · inopON DEPART, RT MLG DOOR APPEAR TO REMAIN OPEN EVEN AFTER CYCLING MLG PER RED TAB PROC. REMOVED AND REPLACED RT GEAR DOOR WARN SWITCH PER MM 32-62-011-4 ADJ & TEST PER MM 32-62-011-5. OPS CK GOOD.Jul 21, 1999 · N144FE · Boeing 72721C · Landing Gear Position and WarningSDR 99FDEA00179Hose · leaks99-113 - LWR AFT BODY O/H LIGHT ILLUM. LIGHT WENT OUT AFTER CLOSE NR 1 BLD AND BEFORE TURN OFF NR 1 PACK. 3RD TIME WRITTEN UP. REMOVED AND REPLACED SENSE LINE. OPER AND LEAK CK NORM.May 14, 1999 · N144FE · Boeing 72721C · Overheat DetectionSDR 99FDEA00178Overheat Loop · inoperative99-112 - LWR AFT BODY LIGHT ILLUM. LIGHT EXTINGUISH WHEN RT PACK AND RT BLD TURN OFF. REMOVED AND REPLACED LOOP PER MM 26-14-001-4. OPER CK NORM.May 13, 1999 · N144FE · Boeing 72721C · Overheat DetectionSDR 99FDEA00175Overheat Light · malfunctionedLOWER AFT BODY O/H LIGHT ON. LIGHT WENT OUT WHEN NR 1 BLD AND LT PACK TURN OFF. INSP DUCT IN AFT AIR STAIRS, CEILING, KEEL BEAM AREA AND NO LEAKS FOUND. COULD NOT DUP O/H COND. OK TO CONTINUE SERVICE.May 12, 1999 · N144FE · Boeing 72721C · Overheat DetectionSDR 99FDEA00005Valve · failedLOWER AFT BODY O/H LIGHT ILLUMINATED. FOLLOWED CK LIST PROCEDURE, CLOSED NR 1 BLEED VALVE AND LEFT PACK. RETARDED NR 1 THROTTLE TO CLIMB POWER. LIGHT REMAINED OUT AND TEST OK, INDICATIVE OF LEAK BETWEEN NR 1 BLEED VALVE AND LEFT PACK VALVE. REMOVED AND REPJan 6, 1999 · N144FE · Boeing 72721C · Pneumatic Distribution SystemSDR 98FDEA00487Bear Strap · corrodedSTA-PAE: CORROSION (C53-224-02) INNER SKIN EMANATING FROM UNDER BEAR STRAP AT BS 475 BETWEEN STRINGER 3 AND 4 LT.Aug 3, 1998 · N144FE · Boeing 72721C · Fuselage Main, Plate/SkinSDR 98FDEA00479Spar Chord · corrodedCORROSION (C53-132-01-1) ON WING CENTER SECTION SPAR CHORD (LOWER) AT BS 745, RBL 12 TO RBL 30, WL 160. *S/D* REMOVED AND REPLACED LOWER SPAR CHORD, BS 745 IAW FED-EX DRAWING 65C21537.Jul 30, 1998 · N144FE · Boeing 72721C · Wing SparSDR 98FDEA00477Spar Chord · corrodedCORROSION (C57-562-02) RT WING SPAR LOWER CHORD HORIZONTAL LEG FS 456 TO 457. *S/D* REPAIRED RT WING FRONT SPAR LOWER SPAR CHORD AT FS 456 TO 467 IAW FED-EX EA 7-5710-35089.Jul 28, 1998 · N144FE · Boeing 72721C · Wing SparSDR 98FDEA00471Web · corrodedWHILE WORKING NR 0840, FOUND CORROSION ON SHEAR WEB BS 1136, RBL 26 TO RBL 44, WL 208 ON UNDER SURFACE OF WEB. *S/D* REPAIRED SHEAR WEB BS 1136, RBL 26 TO RBL 44, WL 208 IAW FED-EX SRM 51-40-2.Jul 23, 1998 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 98FDEA00465Floorbeam · corrodedCORROSION (C53-224-06) IN SEVERAL AREAS ON THE UPPER CHORD OF THE BS 344 FLOORBEAM FROM LBL 63 TO RBL 21. REMOVED, FABRICATED AND INSTALLED FLOORBEAM UPPER CHORD AT BS 344, LBL 65 TO RBL 65 IAW FEDEX SRDM 27-53-007.Jul 23, 1998 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 98FDEA00462Stringer · corrodedCORROSION (C53-224-02) ON STRINGER 9 LT, BS 380 TO 460. *S/D* REPAIRED STR 9 LT, BS 380 TO 480 PER FED-EX SRM 53-10-3.Jul 17, 1998 · N144FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 98FDEA00461Stringer · corrodedCORROSION (C53-224-02) ON STRINGER 1 BL 0 BS 560 TO 580, BS 520 TO 540. *S/D* REMOVED CORROSION FROM STR 1, FOUND IT TO BE OUT OF LIMITS. REPAIRED STR 1, BS 520 TO 540 IAW FED-EX SRM 53-10-3.Jul 17, 1998 · N144FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 98FDEA00366Stringer · corrodedNR 0684 044, CORROSION (C53-224-01(3)) ON STRINGER 2 LT, BS 950-1050. REPAIRED NR 2 LT STRINGER, BS 950-1050 IAW FED-EX SRM 53-10-3.May 27, 1998 · N144FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 98FDEA00121Frame · crackedNR 0926 043, STA-PAE - WHILE WORKING NR 0920 FOUND FRAME BEHIND NR 3 WINDOW ON THE RT SIDE AT BS 254, STR 9-11 RT TO BE CRACKED. REMOVED FRAME RT SIDE AT BS 254, STR 9-11. FABRICATED FRAME FROM 7075-T6.040. ALODINED AND PRIMED. INSTALLED FRAME IAW SRM 51-1Feb 20, 1998 · N144FE · Boeing 72721C · Fuselage Main, FrameSDR 98FDEA00109Skin · crackedNR 0920 042, WHILE PERFORMING HFEC INSPECTION OF FASTENER HOLES. FOUND CRACK EMANATING FROM HOLE AT BS 259.5, STR 8 R. REPAIRED CRACK AT BS 259.5, STR 8R PER EO 7-5330-7-2319G PT5 AND DRAWING 69-62161.Feb 16, 1998 · N144FE · Boeing 72721C · Fuselage Main, Plate/SkinSDR 98FDEA00095Long Beam · corrodedNR 0557 041 STA-PAE - CORROSION (C53-224-01(2)) AROUND NUTCLIP HOLES LBL 45 LONGITUDINAL BEAM BS 838-843, WL 208. REMOVED AND REPLACED LBL 45 LONGITUDINAL BEAM WL 208 FROM BS 740 TO BS 848.5 PER BOEING 727 DRAWING 65-34144.Feb 10, 1998 · N144FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 97FDEA00874Bottle Fitting · corrodedWHILE WORKING NR0748, DISCOVERED CORROSION ON AFT SIDE OF RT BOTTLE FITTING, BS 870, RBL 66, WL 184. *S/D* REMOVED CORROSION, BLENDED ON AFT SIDE OF RT BOTTLE PIN COATING, FOUND COATING TO BE IN LIMITS PER FED EA 7-5710-35103.Dec 3, 1997 · N144FE · Boeing 72721C · Fuselage, Wing Attach FittingsSDR 97FDEA00809Switches · moisture contamRIGHT MAIN GEAR DOOR LIGHT ON SECOND OFFICER'S ANNUNCIATOR PANEL AND RED GEAR DOOR LIGHT ON GEAR POSITION PANEL REMAINED ILLUMINATED AFTER EXTENSION. GEAR INDICATION NORMAL AFTER RECYCLING. INSPECTED DOOR SWITCHES, FOUND SOME MOISTURE, CLEANED WITH CONTACT CNov 7, 1997 · N144FE · Boeing 72724C · Landing Gear Position and WarningSDR 97FDEA00724Skin · corrodedBULGE IN SKIN LAP AT STR 20, BS 1070 LEFT HAND SIDE. *S/D* REMOVED CORROSION AND REPAIRED SKIN LAP AT STR 20 LEFT HAND BS 1070 PER FED-EX SRM 53-30-3 FIG 14.Oct 10, 1997 · N144FE · Boeing 72721C · Fuselage Main, Plate/SkinSDR 97FDEA00717Floorbeam · corrodedCORROSION ON UPPER CHORD OF FLOORBEAM AT BS 312, LBL 30, WL 208. *S/D* FOUND CORROSION TO BE OUT OF LIMITS. REMOVED CORROSION AT BS 312 FLOORBEAM UPPER CHORD LBL 30, WL 208 IAW FED-EX SRM 53-10-8 FED-EX SRM 53-10-1.Oct 9, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00704Skin · corrodedWHILE WORKING NR0768, DISCOVERED CORROSION ON UPPER SKIN IN NR 2 TANK FROM BS 867 TO BS 870, RBL 65 TO LBL 65, WL 190. *S/D* REMOVED CORROSION ON LOWER SURFACE OF UPPER SKIN IN NR 2 TANK FROM BS 867 TO BS 870, RBL 65 TO LBL 65, WL 190 AND REPAIRED PER FED-EX Oct 6, 1997 · N144FE · Boeing 72721C · Fuselage Main, Plate/SkinSDR 97FDEA00697Chord · crackedNR 0706 036 STA-PAE - CORROSION (C53-224-05) CRACK IN RT 70.85 PLUS CHORD IS CRACKED ON UPPER VERTICAL FLANGE IN RADIUS FROM BS 760 TO 770, WL 201, RBL 70.5 LONG CRACK REPAIR REQUIRED PER S/B 727-57-0112 REV 5. REPAIRED CRACK IN RT 70.8 PLUS CHORD PER EA 7-5Oct 1, 1997 · N144FE · Boeing 72721C · Wing Miscellaneous StructureSDR 97FDEA00684Floorbeam · crackedNR 0857 035 WHILE WORKING NR 0822 DISCOVERED BS 328 FLOORBEAM WEB TO BE CRACKED T LBL 30, WL 206. REPAIRED BS 328 FLOORBEAM WEB AT LBL 30, WL 206 AS PER FED-EX SRM 51-40-2.Sep 25, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00683Floorbeam · corrodedNR 0534 034 CORROSION (C53-224-06) AROUND FASTENERS IN THE CARGO TIE DOWN PUCK ON THE BOTTOM OF UPPER FLOORBEAM CHORD AT BS 620, RBL 62.5. REPAIRED UPPER FLOORBEAM CHORD AT BS 620, RBL 15 TO RBL 70 AS PER FED SRM 53-10-8.Sep 25, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00666Casting · corrodedCORROSION (C53-224-06) IN FORWARD POCKET OF THE BARRIER NET CASTING AT RBL 1 TO RBL 8 BS 360 TO BS 380, WL 208. *S/D* REMOVED AND REPLACED BARRIER NET CASTING AT RBL 1 TO RBL 8 BS 360 TO BS 380, WL 208 PER FED-EX SRM 51-30-2. ALODINED AND PRIMED PER FED-EX SSep 18, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00653Skin · corrodedNR 0832 032 CORROSION (C53-224-05) ON WING CENTER TANK UPPER SKIN LBL 46, WL 192, BS 861.5 AND RBL 46, WL 192, BS 861.5. REMOVED CORROSION ON WING CENTER TANK UPPER SKIN, TOP SURFACE AT LBL 46, WL 192, BS 861.5 AND RBL 46, WL 192, BS 861.5 AND REPAIRED PER FESep 12, 1997 · N144FE · Boeing 72721C · Wing, Plate/SkinSDR 97FDEA00650Fitting · corrodedNR 0839 031 CORROSION ON HORIZONTAL SPLICE PLATE AT BS 227, WL 235, LBL 45. REMOVED AND REPLACED HORIZONTAL SPLICE PLATE AT BS 227, WL 235, LBL 45 AS PER FED-EX SRM 51-10-2, 51-10-1, 51-30-2 AND M/M 51-20-151.Sep 11, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00629Fitting · crackedNR 0764 030 FOUND CRACK ON OUTBOARD HOLE OF STRINGER 29R, BS 1103. REMOVED CRACKED STRINGER FITTING. REPLACED WITH A NEW STRINGER FITTING AT BS 1183, STR 29R, IAW FED-EX SRM 51-30-02.Sep 4, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00618Floorbeam · corrodedNR 0822 028 CORROSION (C53-224-06) ON UPPER SURFACE OF TOP CHORD OF FLOORBEAM BS 328, LBL 29-32, WL 208. REPAIRED TOP CHORD OF FLOORBEAM BS 328 FROM LBL 9 TO LBL 63, WL 208 IAW FED-EX SRM 53-10-8.Sep 2, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00617Stringer · corrodedNR 0551 029 CORROSION (C53-224-06) ON STRINGER 9 LEFT IN SEVERAL AREAS BETWEEN BS 620 AND 740. REPAIRED 59L BETWEEN BS 620-740 IAW FED 53-10-1 AND FED SRM 53-10-3.Sep 2, 1997 · N144FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 97FDEA00612Strap · corrodedCORROSION (C53-111-01,3) ON CENTER STABILIZER STRAP FROM BS 988 TO BS 1090, BL 0 WL 200. *S/D* REMOVED AND REPLACED BL 0 BS 950 TO 1158, WL 200 STABILIZER STRAP PER FED-EX SRM 51-10-1 AD 51-30-2.Sep 2, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00601Floorbeam · corrodedNR 0840 020 STA-PAE - WHILE WORKING NR0374 FOUND DOUBLE HOLES IN UPPER SIDE OF BS 1130 CHORD, BS 1130, RBL 32 AND 37, LBL 33 AND 38, WL 208 ALSO CORROSION AND CRACK INDICATION AT LBL 33. REPAIRED UPPER CHORD OF 1130 BEAM IAW FED-EX EA 7-5310-36165 AND EA 7-5Sep 2, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00619Spar Chord · corrodedNR 0748 027 STA-PAE - CORROSION (C57-174-01) ON BS 870 REAR SPAR UPPER CHORD RBL 20-60, LBL 10-40, WL 178. BLENDED, REMOVED CORROSION ON UPPER REAR SPAR CHORD, BS 870, RBL 20-60, LBL 10-40, WL 178. CHORD FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. RESep 1, 1997 · N144FE · Boeing 72721C · Wing SparSDR 97FDEA00616Strap · corrodedNR 0848 023 WHILE WORKING NR 0748 DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD, TENSION LOAD STRAP AT BS 873, WL 177, RBL 65 - LBL 65. REMOVED, FABRICATED AND REPLACED TENSION STRAP AT BS 870, WL 177 FROM RBL 65 TO LBL 65 ON FWD SIDE OF WHEEL WELL Sep 1, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00615Bulkhead Doubler · corrodedNR 0851 024 WHILE WORKING NR 0748, DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD RT RING DOUBLER, AT BS 873, RBL 58, WL 183. REMOVED, FABRICATED AND REPLACED RT RING DOUBLER AT BS 870, RBL 58, WL 183 IAW FED-EX DRAWING 69-14467.Sep 1, 1997 · N144FE · Boeing 72721C · Fuselage Main, BulkheadSDR 97FDEA00614Bulkhead Web · corrodedCORROSION (C57-174-01) ON BS 870 BULKHEAD WEB, RBL 70 - LBL 70, WL 178 TO 138. *S/D* BLENDED, REMOVED CORROSION ON BS 870 BULKHEAD WEB, FOUND TO BE OUT OF LIMITS PER FED SRM 53-10-1. REMOVED AND REPLACED BS 870 BULKHEAD WEB PER FED SRM 51-10-1.Sep 1, 1997 · N144FE · Boeing 72721C · Fuselage Main, BulkheadSDR 97FDEA00613Bulkhead Doubler · corrodedNR 0847 026 WHILE WORKING NR 0748, DISCOVERED CORROSION ON FWD SIDE OF WHEEL WELL BULKHEAD, LEFT RING DOUBLER AT 873, LBL 58, WL 183. REMOVED, FABRICATED AND REPLACED LEFT RING DOUBLER AT BS 870, LBL 58, WL 183 IAW FED-EX DRAWING 69-14467.Sep 1, 1997 · N144FE · Boeing 72721C · Fuselage Main, BulkheadSDR 97FDEA00611Spar · corrodedCORROSION (C57-174-01) ON BS 870 REAR SPAR LOWER CHORD, LBL 40 TO 45, WL 138. *S/D* REMOVED CORROSION, BLENDED ON BS 870 REAR SPAR LOWER CHORD. FOUND CHORD TO BE OUT OF LIMITS PER FED SRM 53-10-1. REMOVED AND REPLACED SPAR CHORD PER EA NR 7-5710-36144.Sep 1, 1997 · N144FE · Boeing 72721C · Wing SparSDR 97FDEA00590Stringer · corrodedNR 0508 018 CORROSION (C53-224-02) ON STRINGER 9 LT, BS 380-460.Aug 27, 1997 · N144FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 97FDEA00589Floorbeam · corrodedCORROSION (C53-111-01(3)) ON LOWER CHORD OF FLOORBEAM AT BS 1130, RBL 26 TO 39, WL 200. *S/D* REPAIRED FLOORBEAM LOWER CHORD IAW FEDEX EA NR 7-5310-36166A.Aug 27, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00582Stringer · corrodedCORROSION (C53-224-02) ON STRINGER 2 RT, BS 480 TO 540, BS 560 TO 580.Aug 26, 1997 · N144FE · Boeing 72721C · Fuselage Main, Longeron/StringerSDR 97FDEA00581Floorbeam · corrodedNR 0229 017 CORROSION (C53-111-01-02) ON FLOORBEAM BS 600, WL 200, LBL 20 TO RBL 25. REPAIRED FLOORBEAM AT BS 600, WL 200, LBL 20 TO RBL 25 IAW FED-EX EA NR 7-5310-35035 REV A.Aug 26, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00579Floorbeam · corrodedCORROSION (C53-224-06) ON NOT CLIP AND DOUBLER UNDER AFT SIDE OF UPPER FLOORBEAM CHORD AT BS 740, RBL 49 AND ON PREVIOUS BLEND OUT UNDER FWD SIDE OF UPPER CHORD AT RBL 47. *S/D* REMOVED OUT OF LIMITS AREAS ON NUTCLIPS AND DOUBLER UNDER AFT SIDE OF UPPER FLOOAug 25, 1997 · N144FE · Boeing 72721C · Fuselage Main, Floor BeamSDR 97FDEA00578Clip · crackedCRACKED STRINGER CLIP BS 970, STR 7 RT. *S/D* DRILLED OUT FASTENERS AND REMOVED CRACKED STRINGER CLIP. POSITIONED NEW STRINGER CLIP INTO PLACE AND BACKDRILL. INSTALLED FAYING SURFACES WET WITH SEALANT AND INSTALLED NEW STRINGER CLIP. ALL WORK DONE PER FEDAug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00577Clip · crackedFOUR EACH CRACKED STRINGER CLIPS AT BS 1010 AT STR 6L, 2R, 7R, 8R. *S/D* REPLACED FOUR EACH STRINGER CLIPS AT BS 1010, STR 6L, 2R, 7R AND 8R PER FED SRM 51-30-2.Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00576Clip · crackedTWELVE EACH CRACKED STRINGER CLIPS AT BS 990 AT STR 8L, 6L, 5L, 4L, 3L, 9R, 8R, 7R, 5R, 4R, 3R AND 2R. * S/D* REMOVED STRINGER CLIPS AND INSTALLED NEW CLIPS AT BS 990, STR 8L, 6L, 5L, 4L, 3L, 9R, 8R, 7R, 5R, 3R, AND 2R PER FED SRM 53-10-1.Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous StructureSDR 97FDEA00575Clip · crackedCRACKED STRINGER CLIP AT BS 970 STR 5 RT. *S/D* REMOVED AND REPLACED STR CLIP AT BS 970, S5R IAW FED SRM 51-10-1 AND SRM 51-30-2.Aug 25, 1997 · N144FE · Boeing 72721C · Fuselage Miscellaneous Structure
Back to N144FE, cancelled Aug 26, 2004