N241FE, cancelled Aug 27, 2013

Service difficulty reports · 155

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 = 'N241FE' AND deregistration_id = 'N241FE-2013-08-27'
  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 FDEA201107303035Flex Hose · leakingAT ABOUT 60-70 KNOTS ON TAKEOFF ROLL S/O CALLED A-SYS HYD QTY WAS ZERO. REJECTED TAKEOFF. PRESSURE ON A SYS WAS NORMAL UNTIL THE RUNWAY CLEARED, THEN LOST HYD PRESSURE. STOPPED ACFT AND SHUTDOWN ENGINES. FOUND A SYS HYD FLEX HOSE FROM THE A SYS HYD MODULE Jul 30, 2011 · N241FE · Boeing 727277 · Hydraulic System, MainSDR FDEA200904301490Stringer Splice · corrodedAFT PIT CORROSION ON STRINGER SPLICE AT BS 1000, STRINGER 29 RT. REMOVED STRINGER SPLICE FOR CORROSION REMOVAL IAW SRM 51-30-2. FABRICATED NEW SPLICE IAW SRM 51-20-2. FIGURE 1 & 51-30-5. INSTALLED NEW STR. SPLICE IAW SRM 51-30-2. APPLIED LEVELING COMPOUND Apr 30, 2009 · N241FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR FDEA200904281461Shear Tie · corrodedFOUND SHEAR TIE CORROSION BS 680 STR 28R TO 28L. CUT-OUT DAMAGED AREA IAW SRM 53-10-4 FIG 15. FABRICATED REPAIR PARTS IAW SRM 53-10-4 FIG 15 AND TREATED AND PRIMED IAW SRM 51-10-2 AND INSTALLED PARTS IAW SRM 53-10-4 FIG 15 AT SHEAR TIE STA 680 STR 28L - 28R.Apr 28, 2009 · N241FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR FDEA200904281460Spar · crackedRIGHT WING T/E FALSE SPAR CHORD ANGLE CRACKED. REMOVED & REINSTALLED TORQUE BOX FITTING TO ACCESS WEB, CUT-OUT DAMAGED AREA. FABRICATED NEW WEB, FABRICTATED NEW CHORD SECTION, FABRICATED 2 ANGLES, FABRICATED 2 RADIUS FILLER, AND FABRICATED NEW DOUBLER. HEATApr 28, 2009 · N241FE · Boeing 727277 · Wing SparSDR FDEA200904271445Spar · crackedLT WING T/E FALSE SPAR LOWER CHORD ANGLE CRACKED, WBL 118. REMOVED DAMAGED SECTION OF FALSE SPAR IAW DWG SR27-57-038. FABRICATED NEW SPAR SECTION, WEB, 2 SUPPORT ANGLES, STRAP, DOUBLER, ALL IAW DWG SR 27-57-038 REV. C. INSTALLED ALL REPAIR PARTS IAW SR 27-57Apr 27, 2009 · N241FE · Boeing 727277 · Wing SparSDR FDEA200904251411Skin · dentedDENT EXTERIOR FUSELAGE STA 712 TO STA 720 6 INCH BETWEEN STR 18R TO STR 19R. CUT OUT DAMAGED AREA, FABRICATED NEW SKIN AND REPAIR DOUBLER. TREATED, PRIMED & INSTALLED NEW PARTS ALL IAW SRM 53-30-3 FIG (12), 51-30-2 & 51-10-2.Apr 25, 2009 · N241FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR FDEA200904251410Skin · misrepairedNON-COMPLIANT REPAIR AT BS 533-543 STR 25R-26R. REMOVED EXISTING REPAIR AND FABRICATED NEW DOUBLER REPAIR, TREATED, PRIMED, & INSTALLED NEW DOUBLER REPAIR ALL IAW SRM 51-30-2, 53-30-3 FIG (1) & 51-10-2.Apr 25, 2009 · N241FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR FDEA200904251409Stringer · corrodedFWD PIT STRINGER 28L CORRODED BS 490. REMOVED FASTENERS AND CUT-OUT DAMAGED AND FABRICATED STRINGER FILLER. FABRICATED NEW SPLICE. TREATED, PRIMED & INSTALLED NEW PARTS ALL IAW 53-10-3 FIG (1), 51-30- 2, AND 51-10-2.Apr 25, 2009 · N241FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR 08FDEA00337Regulator · failedDURING CLIMB-OUT WITH ENG ANTI ICE OPEN, WHEN RT PACK WAS TURNED ON, RIGHT PSI MAXED OUT TO 110 PSI. WHEN RT PACK WAS SWITCHED OFF, ENG 3 STRUT OVHT LIGHT ILLUM FOR APPROX 20 SEC. NR 3 PWR LEVER WAS REDUCED AND LIGHT WENT OUT. CYCLING THE PACK BACK ON PSI RJan 31, 2008 · N241FE · Boeing 727277 · Cabin Cooling SystemSDR 08FDEA00100Switch · damagedAFT AIRSTAIR AMBER WARNING LIGHT ILLUMINATED IN FLIGHT WHILE CRUISING AT FL 350. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CATEGORY: C EXPIRATION: 21JAN08 "MEL 52-06-B: AMBER AFT AIRSTAIR DOOR WARNING LIGHT - INOP." REMOVED AND REPLACED AFT AIRSTAIRSJan 10, 2008 · N241FE · Boeing 727277 · Door Warning SystemSDR 07FDEA02503Rib · damagedCOMPLY WITH EA 7-5710-110753, RT SIDE ONLY, WINGS- (AD 90-06-09 AND AD 94-07-08) MAIN FRAME, RIB UPPER CHORD REPAIR EO 7-5710-7-2308 PART 2. COMPLIED WITH EA 7-5710-110753 RT SIDE IAW SB 727-57-0112.Jul 17, 2007 · N241FE · Boeing 727227 · Wing, Rib/BulkheadSDR 07FDEA02502Rib · misalignedCOMPLY WITH EA NR 7-5710-110754 WING, (AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS. COMPLIED WITH EA NR 7-5710-110754 WING, (AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER REPAIR DEVIATIONS.Jul 17, 2007 · N241FE · Boeing 727227 · Wing, Rib/BulkheadSDR 07FDEA02501Rib · misalignedWING RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS EA NR 7-5710-110754. COMPLIED WITH EA NR 7-5710-110754 WING, AD 90-06-09: 94-07-08: 98-11-03) RBL 70.5 RIB UPPER CHORD REPAIR DEVIATIONS.Jul 17, 2007 · N241FE · Boeing 727227 · Wing, Rib/BulkheadSDR 07FDEA02091Rib · crackedRIGHT RIB CHORD UPPER VERTICAL FLANGE HOLE AT STATION 760.95. LOWER FWD HOLE (B), RELEVANT CRACK INDICATION NOTED AT THE 9 O`CLOCK POSITION LOOKING I/B. MADE TEMPORARY REPAIR PER ENGINEERING AND AIRCRAFT WAS FERRIED TO VENDOR FOR PERMANENT REPAIR.Jun 7, 2007 · N241FE · Boeing 727277 · Wing, Rib/BulkheadSDR 06FDEA04166Stringer · crackedVERTICAL STAB INTERIOR, STR 9 LT IS CRACKED AT RIB STA 110.4 REPAIRED PER FED EX EA 7-5530-100611.Dec 2, 2006 · N241FE · Boeing 727227 · Vertical Stabilizer, Spar/RibSDR 06FDEA04138Skin · corrodedCORROSION LEFT WING UPPER SKIN AT BUTT SPLICE 42" OTBD OF NR 4 SLAT INBD EDGE. REPAIRED PER FED EX EA 7-5730-105911.Nov 29, 2006 · N241FE · Boeing 727227 · Wing, Plate/SkinSDR 06FDEA04021Flap Track · corrodedRT WING LWR SURFACE AT NR 7 FLAP TRACK HAS CORROSION AT FWD TRACK MOUNTING BRACKET. REPAIRED PER FED EX EA 7-5710-100604.Nov 16, 2006 · N241FE · Boeing 727277 · Trailing Edge FlapsSDR 06FDEA04022Shear Tie · corrodedFOUND CORROSION BETWEEN SHEAR TIE AND FRAME BS 1148, STR 28 LT - 30 LT. REPAIRED SHEAR TIE PER SRM 53-10-4 FIG 14.Nov 16, 2006 · N241FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR 06FDEA04020Fitting · corrodedWHILE WORKING CARD N00533, FOUND CORROSION ON NR 5 K-FLAP CENTER HINGE FITTING (A/C SIDE) IB LUG, I/B FACE. REPAIRED NR 5 K-FLAP CENTER HINGE FITTING IAW FED EX EA 7-5710-100605.Nov 16, 2006 · N241FE · Boeing 727277 · Trailing Edge FlapsSDR 06FDEA04014Flap Track · corrodedNR 7 FLAP TRACK HAS CORROSION AT AFT MOUNTING HOLES. REMOVED AND REPLACED NR 7 FLAP TRACK IAW FED EX W/C 27X5709-03.Nov 15, 2006 · N241FE · Boeing 727277 · Trailing Edge FlapsSDR 06FDEA03995Skin · unknownRT STAB UPPER SURFACE, STA APPROX 4" FROM I/B END T/E, EXTERNAL 3" DOUBLERS, REQUIRES EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF THE REPAIR IS IN ACCORDANCE WITH FAA, APPROVED DATA. REMOVED EXISTING REPAIR ON RT HORIZ STAB UPPER SURFACE AND RENov 13, 2006 · N241FE · Boeing 727277 · Horizontal Stabilizer, Plate/SkinSDR 06FDEA03994Angle · corrodedFOUND CORROSION ON UPPER SPOILER BEAM ANGLE FROM NR 5 TO NR 6 SPOILER ACTUATORS. REMOVED DAMAGE ON UPPER SPOILER BEAM ANGLE FROM NR 5 TO NR 6 SPOILER ACTUATORS AND REPAIRED IAW SRM 51-40-4.Nov 13, 2006 · N241FE · Boeing 727277 · SpoilersSDR 06FDEA03986Seat Track · corrodedEXPANSION LINK, BS 740-760, LBL 45 CORRODED AROUND FWD ATTACH BOLT. REMOVED AND REPLACED EXPANSION LINK BS 740-760 LBL 45 IAW SRM 53-10-1.Nov 13, 2006 · N241FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA03941Depressor · damagedAFT NR 2 CARGO DOOR LWR FWD CORNER SEAL DEPRESSOR DAMAGED. REMOVED AND REPLACED AFT NO. 2 CARGO DOOR LWR FWD SEAL DEPRESSOR IAW SRM 51- 30-5.Nov 10, 2006 · N241FE · Boeing 727200 · Cargo/Baggage DoorsSDR 06FDEA03940Depressor · damagedAFT NR 2 CARGO DOOR LWR CENTER SEAL DEPRESSOR CHAFED. REMOVED AND REPLACED AFT NO. 2 CARGO DOOR CNTR SEAL DEPRESSORE IAW SRM 51-30-5.Nov 10, 2006 · N241FE · Boeing 727277 · Cargo/Baggage DoorsSDR 06FDEA03943Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER CHORD BS 380 RBL 50 WL 208. REMOVED DAMAGE AREA OF UPPER CHORDS AT BS 380 RBL 50 AND REPAIRED IAW SRM 53-10-8.Nov 10, 2006 · N241FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA03942Skin · bulgedAFT NR 2 CARGO DOOR SKIN BULGING AROUND 8 CUPPED FASTENERS 1-2 INCHES FROM AFT EDGE 8-10 INCHES FROM BOTTOM. CUT OUT DAMAGE AREA LWR AFT CORNER, FABRICATED SKIN DOUBLER AND FILLER INSTALLED REPAIR ALODINED & PRIMED. REINSTALLED LEVELING COMPOUND PER SRM 52-Nov 10, 2006 · N241FE · Boeing 727277 · Cargo/Baggage DoorsSDR 06FDEA03939Skin · misrepairedNR 2 CARGO DOOR, EXTERNAL SKIN, FWD LWR CORNER, DOUBLER REPAIR REQUIRES EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF THE REPAIR IS IN ACCORDANCE WITH FAA, APPROVED DATA. COMING DOUBLER REPAIR ON NR 2 CARGO DOOR SKIN WAS NOT IN COMPLIANCE WITNov 10, 2006 · N241FE · Boeing 727277 · Cargo/Baggage DoorsSDR 06FDEA03938Frame · dentedFOUND DENT IN FRAME STA 600 BETWEEN STR 24L - 25L. REMOVED DAMAGE IN FRAME STA 600 BETWEEN STR 24L - 25L AND REPAIRED IAW SRM 51-30-2.Nov 10, 2006 · N241FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA03936Frame · damagedFWD CARGO COMPARTMENT, DAMAGE TO STA 520 FRAME BETWEEN STR 22L AND 25L. REMOVED DAMAGE ON FRAME BS 520 BETWEEN STR 22L AND 25L AND REPAIRED IAW SRM 53- 10-1.Nov 9, 2006 · N241FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA03931Frame · dentedFRAME FLANGE DENTED STA 680 STR 23L - 25L. REMOVED DAMAGE ON FRAME BS 680 STR 23L-25L AND IAW SRM 51-40-3.Nov 9, 2006 · N241FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA03935Floorbeam · damagedDRILL START IN UPPER CHORD OF BS 870 FLOORBEAM AT LBL 50, WL 208. REPAIRED BS 870 FLOORBEAM AT LBL 50, WL 208 IAW FED EX EA 7-5310- 105909.Nov 9, 2006 · N241FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA03934Shear Tie · corrodedAFT CARGO BAY CORROSION ON SHEAR TIE BS 1148 LBL 3. REMOVED AND REPLACED SHEAR TIE BS 1148 LBL 3 IAW SRM 53-10-4.Nov 9, 2006 · N241FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR 06FDEA03933Shear Tie · corrodedAFT CARGO BAY CORROSION ON SHEAR TIE BS 1148 LBL 10. REMOVED AND REPLACED SHEAR TIE BS 1148 LBL 10 IAW SRM 53-10-4.Nov 9, 2006 · N241FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR 06FDEA03932Shear Tie · corrodedAFT CARGO BAY CORROSION ON SHEAR TIE BS 1148 LBL 16. REMOVED AND REPLACED SHEAR TIE AT BS 1148 LBL 16 IAW SRM 53-10-4.Nov 9, 2006 · N241FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR 06FDEA03923Shear Web · damagedWHILE WORKING N01197 FOUND LT SHEAR WEB AT BS 1130 - 1176, LBL 25 - LBL 65, WL 208 TO HAVE NUMEROUS MISDRILLED AND DOUBLE HOLES. REMOVED AND REPLACED LEFT SHEAR WEB AT BS 1130 - BS 1176, LBL 25 - LBL 65 WL 208 PER SRM 51-30-2.Nov 8, 2006 · N241FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR 06FDEA03920Crease Beam · corrodedFOUND CORROSION ON CREASE BEAM WEB AT BS 720C PLUS 11" AND 720C PLUS 18", LBL 65, WL 208. REMOVED DAMAGE ON CREASE BEAM AT 720C PLUS 11 TO 720C PLUS 18, LBL 65, WL 208 AND REPAIRED IAW SRM 51-30-2.Nov 8, 2006 · N241FE · Boeing 727277 · Fuselage Main, StructureSDR 06FDEA03926Crease Beam · damagedFOUND CREASE BEAM TO BE MISDRILLED AT BS 720F AND 720E LBL 63, WL 208. REMOVED DAMAGE CREASE BEAM AT BS 720F TO 720E LBL 63 WL 208 AND REPAIRED IAW SRM 51-30-5, 51-30-6, AND 51-30-8.Nov 8, 2006 · N241FE · Boeing 727277 · Fuselage Main, StructureSDR 06FDEA03924Spar · damagedSHEARED FASTENER HEAD IN RT WING UPPER REAR SPAR VERTICAL FLANGE AT WS 212. REPAIRED PER FED EX EA 7-5710-100602.Nov 8, 2006 · N241FE · Boeing 727277 · Wing SparSDR 06FDEA03922Shear Web · crackedWHILE WORKING 1176 CHORD, FOUND AFT CENTER SHEAR WEB FROM BS 1148 - BS 1176, LBL 25 - RBL 25, WL 208 TO HAVE NUMEROUS DOUBLE HOLES AND TO BE CRACKED. FABRICATED NEW WEB PER SRM 51-0-2.Nov 8, 2006 · N241FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR 06FDEA03921Shear Web · dentedFOUND DENT IN SHEAR WEB AT BS 1137, RBL 26, WL 208. REPAIRED PER SRM 51-40-2 FIG 1.Nov 8, 2006 · N241FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR 06FDEA03911Crease Beam · corrodedFOUND CORROSION ON CREASE BEAM WEB BS 720D - BS 720E, STR 17L. REMOVED DAMAGED CREASE BEAM WEB BS 720D-720E, STR 17L AND REPAIRED IAW SRM 51-10-2.Nov 7, 2006 · N241FE · Boeing 727277 · Fuselage Main, StructureSDR 06FDEA03910Skin · damagedE/E BAY DOOR OUTER SKIN DAMAGED ALL AROUND OUTER EDGE, AFT LT, OUT OF LIMITS. REMOVED AN AREA APX 3" BY 16" FROM AFT LT EDGE SKIN OF E/E BAY DOOR. FABRICATED FILLER FROM 2024-T3 .040, LOT 707522 AND PATCH FROM 2024-T3, 050, LOT NR 715012 PER SRM 52-00-3, FIGNov 7, 2006 · N241FE · Boeing 727277 · Electrical/Electronic Compartment DoorsSDR 06FDEA03913Frame · crackedOUTER CHORD OF FRAME CRACKED STA 804.5 STR 14R. REMOVED AND REPLACED OUTER CHORD OF FRAME 804.5 STR 14R IAW SRM 51-30-5, 51-30-2.Nov 7, 2006 · N241FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA03912Frame · dentedFRAME FLANGE DENTED STA 660 STR 23L - 25L. DENT ON FRAME FLANGE BS 660 STR 23L - 25L FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE OF FRAME LOCATED DRILLED NEW FRAME SECTION ALODINED, PRIMED AND INSTALLED SRM 53-10-1, SRM 51-40-3.Nov 7, 2006 · N241FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA03909Stiffener · corrodedWHILE WORKING ON THE L/W UPPER SKIN CORROSION AT THE FRONT SPAR WING LBL 348, FOUND THE TEE CLIP COMMON TO THE UPPER SPAR CHORD AND WSTA 357 RIB FWD STIFFENER CRACKED. REMOVED AND REPLACED TEE CLIP AT L/W STE 357 IAW SRM 51-30-5, 51-30-6, 51-30-2.Nov 7, 2006 · N241FE · Boeing 727277 · Wing Miscellaneous StructureSDR 06FDEA03908Stiffener · corrodedWHILE WORKING ON THE L/W UPPER SKIN CORROSION AT THE FRONT SPAR WING LBL 348, FOUND THE TEE CLIP COMMON TO THE UPPER SPAR CHORD AND WSTA 410 RIB FD STIFFENER CORRODED. REMOVED AND REPLACED TEE CLIP AT L/W STA 410 IAW SRM 51-30-5, 561-30-6, 51-30-2.Nov 7, 2006 · N241FE · Boeing 727277 · Wing Miscellaneous StructureSDR 06FDEA03907Stringer · crackedFOUND STR 16L IS CRACKED AT BS 644. REMOVED DAMAGED AREA, LOCATED AND DRILLED REPAIR PARTS AND INSTALLED IAW SRM 53-10-3.Nov 7, 2006 · N241FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR 06FDEA03899Shear Tie · corrodedFOUND CORROSION C53-111-01, ON FRAME SHEAR TIE STA 720A BETWEEN STR 27L - 28L. REMOVED SHEAR TIE FABRICATED NEW SHEAR TIE ALODINIED AND PAINTED PARTS INSTALLED WET WITH SEALANT PER SRM 51-10-1, SRM 53-10-4, SRM 51-30-2, SRM 51-20-4 AT STA 720A BETWEEN STR 27LNov 6, 2006 · N241FE · Boeing 727277 · Fuselage Internal Mounting StructureSDR 06FDEA03854Frame · dentedFOUND DENT ON FRAME AT BS 520 STR 126R.Nov 2, 2006 · N241FE · Boeing 727277 · Fuselage Main, Frame
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