N153FE, cancelled Dec 4, 2006

Service difficulty reports · 36

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 = 'N153FE' AND deregistration_id = 'N153FE-2006-12-04'
  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 97FDEA00379Light · inoperativeFWD ENTRY DOOR EMERGENCY EXIT LIGHT IS INOP. *S/D* REMOVED AND REPLACED FWD ENTRY DOOR EMERGENCY EXIT LIGHT AND PERFORMED OPERATIONAL TEST IAW FED-EX M/M 33-50-101.Jul 1, 1997 · N153FE · Boeing 72725 · Emergency LightingSDR 97FDEA00378Hinge · corrodedNR 0328 033 STA-PAE - R/W O/B AILERON CENTER O/B HINGE FITTING ON AIRCRAFT IS CORRODED (REQUIRES AILERON REMOVAL). REMOVED R/W O/B AILERON. REMOVED AND REPLACED R/W O/B AILERON, O/B HINGE FITTING. REINSTALLED R/W O/B AILERON ALL WORK DONE IAW FED-EX M/M 27Jun 23, 1997 · N153FE · Boeing 72725 · AileronsSDR 97FDEA00377Light · inoperativeCONTROL CABIN EMERGENCY EXIT LIGHT IS INOP. *S/D* REMOVED AND REPLACED MOUNTING PLATE FOR EMERGENCY EXIT LIGHT ASSY IN COCKPIT IAW FED-EX WDM 33-51-01. PERFORMED SATISFACTORY TEST IAW FED-EX M/M 33-50-0.Jun 23, 1997 · N153FE · Boeing 72725 · Emergency LightingSDR 97FDEA00363Hinge · corrodedSTA-PAE: RT WING O/B AILERON CENTER O/B HINGE FITTING ON AIRCRAFT IS CORRODED (REQUIRES AILERON REMOVAL). *S/D* REMOVED RT WING O/B AILERON. REMOVED AND REPLACED RT WING O/B AILERON, O/B HINGE FITTING. REINSTALLED RT WING O/B AILERON. ALL WORK DONE IAW FJun 23, 1997 · N153FE · Boeing 72725 · AileronsSDR 97FDEA00351Skin · crackedNR 0745, FASTENER HOLE ON EXTERIOR SKIN HAS CRACK INDICATION BS 220, WL 220, LBL 45. *S/D* REPAIRED FASTENER HOLE ON EXTERIOR SKIN AT BS 220, WL 220, LBL 45 PER FED-EX SRM 53-30-3 AND EO 7-5330-7-2338 PT 1.Jun 17, 1997 · N153FE · Boeing 72725 · Fuselage Main, Plate/SkinSDR 97FDEA00348Frame · crackedNR 0739 031, BS 1253 FRAME IS CRACKED AT LBL 3 TO LBL 5, WL 368 FRAME LOCATED IN NR 2 ENGINE AIR INLET HOUSING. *S/D* REMOVED DAMAGE, FABRICATED REPAIR PARTS, ALODINED AND PRIMED REPAIR PARTS. INSTALLED REPAIR PARTS BS 1253, LBL 7 TO RBL 2, WL 368 PER FED-EXJun 15, 1997 · N153FE · Boeing 72725 · Fuselage Main, FrameSDR 97FDEA00334Chord · corrodedNR 0287 030 CORROSION ON BS 1176 CHORD RBL 2- RBL 42, WL 208. REMOVED AND REPLACED BS 1176 CHORD WL 208 PER FED-EX SRM 51-10-1.Jun 8, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00330Bulkhead Web · crackedNR 0759 029, NUMEROUS CRACKS IN 950 BULKHEAD WEB, LBL 60, WL 188 TO 199.Jun 7, 1997 · N153FE · Boeing 72725 · Fuselage Main, BulkheadSDR 97FDEA00321Door Frame · corrodedNR 0473 027, CORROSION ON DOOR FRAME DOUBLER AT BS 425.Jun 4, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00320Keel Beam · corrodedNR 0117 028, CORROSION ON LT KEEL BEAM AT BS 1055 TO 1065 ON OUTBOARD FLANGE LBL 7.Jun 4, 1997 · N153FE · Boeing 72725 · Fuselage Main, KeelSDR 97FDEA00319Tension Strap · corrosionNR 0716 025, WHILE WORKING NR0476, DISCOVERED CORROSION ON WHEEL WELL FWD BULKHEAD TENSION STRAP LBL 25 TO 70.5, RBL 30 TO 70.5 AROUND FASTENERS. *S/D* REPAIRED WHEEL WELL FWD BULKHEAD TENSION STRAP LBL 25 TO 70-5 AND RBL 30 -TO 70.5 PER EA NR 7-5310-34024Jun 2, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00317Stringer · corrodedNR 0644 024 CORROSION (C53-111-01(3)) ON STRINGER FITTING ON UPPER AND LOWER O/B FLANGE STR 20 LT, BS 1154-1163. REMOVED AND REPLACED STRINGER FITTING STR 20 LT, BS 1154-1163 IAW FED-EX SRM 51-30-2.May 30, 1997 · N153FE · Boeing 72725 · Fuselage Main, Longeron/StringerSDR 97FDEA00315Stiffener · corrodedNR 0470 023, CORROSION (C53-111-01) ON WHEEL WELL VERIFIED STIFFENER BS 320, RBL 14, WL 170. *S/D* REMOVED AND REPLACED VERTICAL STIFFENER AT BS 320, RBL 14, WL 170 IAW FED-EX SRM 51-30-2.May 29, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00310Floorbeam · corrosionNR 0633 022, WHILE WORKING NR 0293, UPON REMOVAL OF LAV WALL HAT CHANNEL FOUND MISDRILLED HOLES AND CORROSION AT BS 344, RBL 53, WL 208 AND CORROSION AT BS 344, RBL 36, WL 208. *S/D* REMOVED DAMAGE, FABRICATED AND INSTALLED FLOORBEAM TOP CHORD AT BS 344, RBLMay 27, 1997 · N153FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 97FDEA00305Floorbeam · corrodedNR 0388 021, CORROSION ON FLOORBEAM BS 360, LBL 5, WL 208. *S/D* REMOVED CORROSION ON FLOORBEAM BS 360, LBL 5, WL 208. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-8.May 25, 1997 · N153FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 97FDEA00306Former · corrodedNR 0737 020, WHILE ACCESSING RT KEEL BEAM FOUND LOWER SKIN FORMER CHORD TO BE BADLY CORRODED AT RBL 10, WL 140, BS 950. *S/D* REMOVED AND REPLACED SKIN FORMER CHORD IAW FED-EX SRM 51-30-2, 51-10-6, AND FED-EX M/M 51-20-0.May 23, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00293Tank Skin · corrosionNR 0733 019 , WHILE WORKING ON (NR0716) FOUND CORROSION ON LOWER TANK, INTERIOR SKIN STA 868 TO 870, RBL 60-LBL 60, WL 139. *S/D* BLENDED AND REMOVED CORROSION, ON LOWER TANK SKIN. FOUND SKIN IS IN LIMITS PER FED-EX 727 SRM 57-30-1 FIG 4. REWORKED SKIN PERMay 18, 1997 · N153FE · Boeing 72725 · Fuel StorageSDR 97FDEA00292Tank Skin · corrosionNR 0734 018, WHILE WORKING ON (NR0474) FOUND CORROSION ON UPPER CENTER TANK (INTERIOR SKIN) STA 868 TO 870, RBL 60-LBL 60, WL 178. *S/D* BLENDED AND REMOVED CORROSION ON UPPER TANK SKIN. FOUND SKIN IS IN LIMIT PER FED-EX SRM 727, 57-30-1 FIG 4. REWORKED SKMay 18, 1997 · N153FE · Boeing 72725 · Fuel StorageSDR 97FDEA00291Spar Chord · corrosionCORROSION (C53-132-02,1) ON UPPER REAR SPAR CHORD STA 870, RBL 65, LBL 65, WL 178. *S/D* REMOVED AND REPLACED UPPER SPAR CHORD STA 870, RBL 65, LBL 65, WL 178 PER FED-EX NR 7-5710-34044.May 18, 1997 · N153FE · Boeing 72725 · Wing SparSDR 97FDEA00290Spar Chord · corrodedNR 0476 016, CORROSION (SPEC C53-132-02,1) ON STA 870 LOWER REAR SPAR CHORD RBL 25, LBL 25, WL 138. *S/D* REMOVED DAMAGED LOWER REAR SPAR CHORD FROM RBL 70 TO LBL 70, WL 138, BS 870 AND INSTALLED NEW LOWER CHORD PER FED-EX EA 7-5710-34044.May 18, 1997 · N153FE · Boeing 72725 · Wing SparSDR 97FDEA00289Bulkhead Web · corrosionNR 0475 015, CORROSION (SPEC C53-132-02,1) ON STA 870 BULKHEAD WEB RBL 65 TO LBL 65, WL 178. *S/D* REMOVED DAMAGED BULKHEAD STA 870, WEB RBL 65 TO LBL 65 AND INSTALLED NEW WEB PER FED-EX EA 7-5710-34044.May 18, 1997 · N153FE · Boeing 72725 · Fuselage Main, BulkheadSDR 97FDEA00284Keel Beam · corrodedNR 0116 014, CORROSION ON RT KEEL BEAM AT BS 973, RBL 7, WL 138. *S/D* REMOVED AND REPLACED RT KEEL BEAM AT BS 960, RBL 17, WL 138 IAW SB 727-53-0179.May 17, 1997 · N153FE · Boeing 72725 · Fuselage Main, KeelSDR 97FDEA00286Floorbeam · corrodedNR 0621 013, WHILE WORKING NR 0440 FOUND CORROSION ON FLOORBEAM BS 560, RBL 45, WL 208 UNDER SEAT TRACK. *S/D* REMOVED CORROSION AT BS 560, RBL 45, WL 208 ON FLOORBEAM UNDER SEAT TRACK FOUND TO BE OUT OF LIMITS IAW 727 FED-EX SRM 53-10-02. REPAIRED DAMAGED May 15, 1997 · N153FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 97FDEA00280Chord · corrodedNR 0471 008, CORROSION (C53-111-01) ON LT MID NOSE CHORD HORIZONTAL FLANGE LOWER SIDE BS 294 TO 350 LBL 15 WILL REQUIRE REMOVAL OF THE FLOOR WEB AND A/C DUCTING TO GAIN ACCESS. *S/D* REMOVED AND REPLACED LT MID NOSE CHORD BS 294 TO 350, WL 169, LBL 15 FED-EXMay 14, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00277Frame · corrodedNR 0465 011, FWD CARGO BS 560 TO STR 22L, FRAME CORRODED UNDER SIDEWALL SUPPORT CH. *S/D* MECHANICALLY REMOVED CORROSION BS 560, STR 22L ON AREA OF 1 BY 1.0397. REMOVED .008 FROM .056 MATERIAL. OUT OF LIMITS PER SRM 53-10-4. REPAIRED FRAME IAW FED-EX SRM May 14, 1997 · N153FE · Boeing 72725 · Fuselage Main, FrameSDR 97FDEA00279G-Beam · corrodedNR 0652 009, WHILE WORKING NR 0506 FOUND CORROSION ON 25 G-BEAM AT BS 266.May 13, 1997 · N153FE · Boeing 72725 · Fuselage Structure (General)SDR 97FDEA00278Floorbeam · corrodedNR 0659 010, CORROSION (C53-111-0, 2) ON LOWER CHORD OF FLOORBEAM BS 600, LBL 18 TO RBL 18, WL 200. *S/D* REPAIRED LOWER CHORD OF FLOORBEAM AT BS 600, LBL 23, RBL 30 IAW FED-EX SRM 53-10-8.May 13, 1997 · N153FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 97FDEA00285Floorbeam · corrodedNR 0390 012, CORROSION (C53-224-02) ON FLOORBEAM BS 620, WL 208, LBL 7 TO LBL 21 AND AROUND NUT PLATE AT LBL 47. *S/D* WHILE REMOVING CORROSION FOUND CRACK IN UPPER CHORD IN EXISTING REPAIR AT LBL 20, STA 620 TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOMay 11, 1997 · N153FE · Boeing 72725 · Fuselage Main, Floor BeamSDR 97FDEA00276Beam · corrodedNR 0520 005, CORROSION EMANATING FROM UNDER SEAT TRACK ON RBL 24 LONGITUDINAL BEAM BS 760 TO 815, WL 208.1. *S/D* REMOVED AND REPLACED LONGITUDINAL BEAM BS 760 TO 848, RBL 24, WL 208 PER FED-EX SRM 53-10-01.May 11, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00274Intercostal · corrodedNR 0508 007, CORROSION (C53-221-01) ON INTERCOSTAL BETWEEN BS 268 TO 277, LBL 15.May 11, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00272Frame · corrodedNR 0517 004, CORROSION (C53-221-01) ON BS 251.6 FRAME WEB LBL 45, WL 215. *S/D* REPAIRED FRAME WEB AT BS 251.6, LBL 45, WL 215 PER FED-EX SRM 51-40-2 DUE TO CORROSION BEING OUT OF LIMITS PER FED-EX SRM 53-10-1.May 11, 1997 · N153FE · Boeing 72725 · Fuselage Main, FrameSDR 97FDEA00271Intercostal · corrodedNR 0509 003, CORROSION (C53-221-01) ON INTERCOSTAL BETWEEN BS 259 TO 277, WL 208, LBL 10. *S/D* REMOVED CORROSION ON INTERCOSTAL AT BS 259 TO 277, LBL 10, WL 208. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED, FABRICATED AND REPLACED INTERCOSTAMay 11, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00270Intercostal · corrodedNR 0507 002, CORROSION (C53-221-01) ON INTERCOSTAL BETWEEN BS 268 AND 274.May 11, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00269Intercostal · corrosionNR 0506 001, CORROSION (C53-221-01) ON INTERCOSTAL BETWEEN BS 280 TO 294, RBL 15, WL 208. *S/D* REMOVED AND REPLACED INTERCOSTAL/FLOOR SUPPORT AT BS 277 TO 294, RBL 15, WL 208, DUE TO CORROSION BEING OUT OF LIMITS. WORK PERFORMED IAW FED-EX SRM 53-30-2 AND May 11, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous StructureSDR 97FDEA00322Beam · corrosionNR 0542 026, CORROSION (C55-391-20, 2) RT HORIZONTAL STAB UPPER TIE BEAM HAS AN AREA OF CORROSION 138 FROM INBOARD END LWR FWD SIDE. * S/D* REMOVED AND REPLACED RT HORIZONTAL STAB UPPER TRAILING EDGE BEAM IAW FED-EX SRM 51-30-5.May 10, 1997 · N153FE · Boeing 72725 · Horizontal Stabilizer StructureSDR 97FDEA00275Beam · corrodedNR 0446 006, CORROSION ON LONGITUDINAL BEAM BS 740 TO 848, LBL 45, WL 208.1. *S/D* REMOVED AND REPLACED LONGITUDINAL BEAM BS 740 TO 848, LBL 45, WL 208.1 IAW FED-EX SRM 51-30-2.May 10, 1997 · N153FE · Boeing 72725 · Fuselage Miscellaneous Structure
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