N269FE, cancelled Aug 22, 2014

Service difficulty reports · 82

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 = 'N269FE' AND deregistration_id = 'N269FE-2014-08-22'
  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 FDEA201206212285Seal · failedAIRPLANE COULD ONLY HOLD STABLE CABIN PRESSURE UP TO 24,000 FT WITH AUTO PRESSURE CONTROLLER SET AT 24,000 FT, CABIN ALTITUDE SHOULD HAVE BEEN 1,000 FT BUT WAS 6,100 FT WITH A 6.2 DIFFERENTIAL AND CARGO HEAT OUTFLOW VALVE CLOSED. PERFORMED PRESSURIZATION CHJun 21, 2012 · N269FE · Boeing 727233 · Passenger/Crew DoorsSDR FDEA201205221933Unknown · unknownPRESSURIZATION SYS NOT FUNCTIONING PROPERLY. COULD NOT GET MORE THAN 6.0 PSID, 9600FT CABIN ALT AND SLOWLY CLIMBING AT FL330. DECENDED TO FL270, DIFFERENTIAL REDUCED TO 5.0 PSI CARGO HEAT VALVE CLOSED FULL TIME AT 10,000FT, CABIN ALT= 5500, DIFFERENTIAL 1May 22, 2012 · N269FE · Boeing 727233 · Cabin Pressure Control SystemSDR FDEA201108043091Skin · corrodedFWD PIT, REMOVED SOFT SEALANT BTW BS 720C - 720D BTW STR 28L - STR 28R EVIDENCE OF CORROSION. REMOVED CORROSION ON SKIN IAW B727 SRM 51-10-6. ORIGINAL MAT. 0.072", REMAINING MAT. 0.054", MAT. LOSS 0.018". FOUND TO BE WITHIN LIMITS IAW EA 7-5330-136797.Aug 4, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201108023094Skin · misrepairedFUSELAGE SKIN HAS FASTENERS WITH IMPROPER SPACING, STA 420-440 BELOW STR 4L. TRIMMED UPPER AND LOWER SKIN AREA BETWEEN STA 420 TO STA 440, STR 4L, FABRICATED FREEZE PLUGS, DOUBLER, FILLER, TAPERED FILLER, TWO FILLER INTERNAL SKIN AND INSTALLED REPAIR PARTAug 2, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201108023077Skin · corrodedFUSELAGE SKIN AT BS 720B, 18" STR 27L HAS EXFOLIATION. CUT OUT DAMAGED AREA OF SKIN, FABRICATED REPAIR DOUBLER AND NEW TEE SUPPORT, AND INSTALLED NEW TEE SUPPORT AND DOUBLER IAW EA 7-5330-136797.Aug 2, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201108023093Skin · misrepairedFUSELAGE SKIN HAS FASTENERS WITH IMPROPER SPACING, STA 440-460 BELOW STR 4L. TRIMMED UPPER AND LOWER SKIN AREA BETWEEN STA 440 TO STA 460, STR 4L, FABRICATED DOUBLER, FILLER , TWO FILLER INTERNAL SKIN AND INSTALLED REPAIR PARTS IAW EA 7-5330-136790.Aug 2, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201108013059Support Angle · corrodedFWD PIT BS 740 LOWER SUPPORT ANGLE HAS CORROSION, LOWER SURFACE AFT OF STR 27L. REMOVED AND REPLACED SUPPORT ANGLE AT BS 740 IAW SRM 51-30-5 AND 51-30-2 REV 103 AND DWG 69-43695.Aug 1, 2011 · N269FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201107313045Seat Track · corrodedSEAT TRACK CORRODED STA 760-848, RBL 45.5. REMOVED SEAT TRACK, FABRICATED SEAT TRACK AND INSTALLED SEAT TRACK IAW SRM 51-10-6, 53-10-1 FIG 3, 51-10-2, 53-10-5 FIG 2 AND 51-30-2.Jul 31, 2011 · N269FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201107262944Shear Tie · corrodedFWD PIT FRAME, BS 720C, AFT SHEAR TIE IS CORRODED BETWEEN STRINGERS 26-27R. REMOVED SHEAR TIE IAW SRM 51-30-2. LOCATED AND DRILLED NEW SHEAR TIE IAW SRM 51-30-2. INSTALLED NEW SHEAR TIE IAW SRM 51-30-2, REV 103.Jul 26, 2011 · N269FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR FDEA201107222890Support Angle · corrodedBS 740 ANGLE IS CORRODED WITH EXFOLIATION BETWEEN STRINGER 28R AND 27R. REMOVED SUPPORT ANGLE IAW SRM 51-30-2 REV 103. FABRICATED NEW ANGLE IAW SRM 51-20-1 FIG 7 AND 51-30-5. INSTALLED SUPPORT ANGLE IAW SRM 51-30-2 AND DWG 69-64841Jul 22, 2011 · N269FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201107212871Shear Tie · corrodedCORROSION ON SHEAR TIE AT BS 700, INBD OF STRINGER 28L. CUT OUT DAMAGED SHEAR TIE IAW SRM 51-10-1. FABRICATED SHEAR TIE DOUBLER IAW SRM 53-10-4 FIG 15. INSTALLED SHEAR TIE REPAIR DOUBLER IAW SRM 53-10-4 FIG 15 REV 103.Jul 21, 2011 · N269FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR FDEA201107192811Spar · crackedCENTER TANK REAR SPAR UPPER WEB BL 0 TO LBL 2 HAS UT SHEAR WAVE CRACK INDICATION AND BL 0 TO RBL HAS HFEC CRACK INDICATION. STOP DRILLED HOLES AT CENTER TANK REAR SPAR UPPER WEB LBL 0-2 AND RBL 0-2 IAW SRM 51-10-1. LOCATED AND DRILLED HOLES AT REPAIR KIT AND Jul 19, 2011 · N269FE · Boeing 727233 · Fuselage Main, FrameSDR FDEA201107192810Skin · gougedMCD INNER SURROUND SKIN GOUGED STA 620, STR 8L. REMOVED DAMAGED INNER SKIN, FABRICATED AND INSTALLED NEW INNER SKIN IAW SRM 53-10-2. FIG 3A AND SRM 51-30-2.Jul 19, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201107192809Skin · corrodedSKIN BULGE STA 440, STR 20R. CUTOUT DAMAGED SKIN -DAMAGED AREA, FABRICATED REPAIR SKIN, REINFORCING STRAPS, SPLICE PLATE AND TAPERED FILLER AND INSTALLED REPAIR SKIN, REINFORCING STRAPS, SPLICE PLATE AND TAPERED FILLER IAW SRM 53-30-3 FIG 12.Jul 19, 2011 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201107152717Torque Box · crackedAFT AIRSTAIR AREA - LIGHTNING HOLE IS CRACKED AT RT LOWER TORQUE BOX BS 1223. CUT OUT DAMAGED WEB IAW SRM 51-10-1 REV 103. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2 AND SRM 51-40-2.Jul 15, 2011 · N269FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA201107152716Torque Box · crackedAFT AIRSTAIR AREA - LIGHTNING HOLE IS CRACKED AT RT LOWER TORQUE BOX BS 1233. CUT OUT DAMAGED WEB IAW SRM 51-10-1 REV 103. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 AND 53-10-2 FIG 6. INSTALLED REPAIR DOUBLER IAW SRM 51-30-2Jul 15, 2011 · N269FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200907142620Accessory Unit · failedAFTER TAKE OFF, THE LANDING GEAR LEVER LATCH FAILED TO RELEASE. LANDING GEAR LEVER COULD ONLY BE RAISED TO OFF POSITION. HORN SOUNDED WHEN FLAPS RETRACTED FROM 5 DEG. TO 2 DEG. REMOVED AND REPLACED M831 AIR SENSING SENSOR PER AMM 32-09-221-4 AND PERFORMJul 14, 2009 · N269FE · Boeing 727233 · Landing Gear Retraction/Extension SystemSDR FDEA200902120510Door Frame · crackedCORRECTION OF SDR 09-0481 FWD CARGO DOORWAY STA 620 LOWER INNER CHORD CRACKED. FABRICATED CHORD ON MAE TRAVELER T9/778261. FABRICATED SPLICE ON MAE TRAVELER T9/779262. CHORD REMOVED AND NEW INSTALLED IAW SRM 51-30-2 AND SRM 51-40-4. MAJOR REPAIR, RII, RDFeb 12, 2009 · N269FE · Boeing 727233 · Fuselage Main, StructureSDR FDEA200902090484Stringer · corrodedFWD CARGO AREA BS 720F TO 740 S-26L STRINGER SEVERAL ROW OF RIVETS CORRODED REPAIRED STRINGER IAW SRM 53-10-3. FABRICATED STRINGER ON MAE TRAVILER T9/778825. MAJOR REPAIR, RII, RDR AND SDR.Feb 9, 2009 · N269FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA200902070482Seat Track · corrodedMCD SEAT TRACK FLANGE HAS CORROSION AT LBL24 APPROX FROM STA 370 TO 460. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-10-5. FABRICATED TRACK AND SPLICES ON MAE TRAVELER T9/779235 AND T9/779236. MAJOR REPAIR, RII, RDR AND SDR.Feb 7, 2009 · N269FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200902070481Structure · crackedFWD CARGO DOORWAY STA 620 LOWER INNER CHORD CRACKED. FABRICATED CHORD ON MAE TRAVELER T9/778261. FABRICATED SPLICE ON MAE TRAVELER T9/779262. REPAIRED CHORD IAW SRM 53-10-2. MAJOR REPAIR, RII, RDR AND SDR.Feb 7, 2009 · N269FE · Boeing 727233 · Fuselage Main, StructureSDR 07FDEA00910Door · unsecureAFTER TAKEOFF IN IAD CABIN ALTITUDE WENT ABOVE 10,00 0' RAN QRH PROCEDURES CABIN ALTITUDE WENT TO 11,500' WENT ON O2 RETURNED TO IAD. NOTICE FORWARD ENTRY DOOR WAS NOT SEATED PROPERLY OPEN AND SECURED DOOR SEVERAL TIMES, PERFORMED FORWARD ENTRY DOOR INSPECTMar 15, 2007 · N269FE · Boeing 727233 · Passenger/Crew DoorsSDR 06FDEA03917Friction Brake · out of adjustON T/O AND CLIMB NR 2 THROTTLE CONSTANTLY CREEPS FORWARD 3-4% N1. THROTTLE NEEDS TO BE CONSTANTLY PULLED BACK NOT TO OVERSPEED ENGINE. ADJUSTED NR 2 ENG FRICTION BRAKE PER 727-200 M/M 76-11-001-8. OPS CHECKED NORMAL.Nov 8, 2006 · N269FE · Boeing 727233 · Power LeverSDR 06FDEA03577Throttle · unknownAFTER LEVEL OFF AT FL 320, F/O NOTED THE NR 2 THROTTLE MOVED ITSELF TO FIREWALL POWER WHILE THROTTLES 1 AND 3 REMAINED AT CLIMB POWER. IMMEDIATELY RETARDED THE THROTTLE BACK TO MATCH 1 AND 3. EPR ON NR 2 WAS 2.57 AND TEMP EXCEEDED 650 DEG. OVERBOOST APPROX Oct 3, 2006 · N269FE · Boeing 727233 · Power LeverSDR 06FDEA2315Attach Fitting · corrodedCORROSION ON FWD ATTACH FITTING AT NR 3 FLAP TRACK.Jun 15, 2006 · N269FE · Boeing 727200 · Trailing Edge FlapsSDR 06FDEA2256Frame · misdrilledDOUBLE HOLE AT BS 600 STR 21L. COMPLIED WITH FED EX EA 7-5310-102255.Jun 8, 2006 · N269FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2255Frame · misdrilledDOUBLE HOLE AT BS 520 STR 21L. COMPLIED WITH FED EX EA 7-5310-102255.Jun 8, 2006 · N269FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2254Frame · misdrilledDOUBLE HOLE AT BS 500 STR 21L. COMPLIED WITH FED EX EA 7-5310-102255.Jun 8, 2006 · N269FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2247Beam · corrodedWHILE WORKING CARD N00862, FOUND CORROSION AT WBL 206, LOWER CHORD OF SPOILER BEAM LOWER SURFACE, RIGHT WING. *S/D* REPAIRED CORROSION RIGHT WING LOWER CHORD OF SPOILER BEAM LWR SURFACE AT WBL 206 IAW FED EX EA 7-5710-100546.Jun 7, 2006 · N269FE · Boeing 727200 · SpoilersSDR 06FDEA2246Web · misdrilledWHILE WORKING CUST CARD N00346 FOUND LOWER SIDE OF THE FLOOR WEB AT BS 1175 RBL 26 WL 208 FASTENER HOLES -SNOWMANNED-. REPAIRED FLOOR WEB AT BS 1175, RBL 26, WL 208 IAW SRM 53-10-1 FIG 1.Jun 7, 2006 · N269FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA2248Skin · dentedMAIN CARGO DOOR EXTERNAL SKIN DENTED 20 INCHES FROM AFT EDGE AND 47 INCHES FROM BOTTOM EDGE. REPAIRED DENT PER FED EX EA 7-5230-102256.Jun 7, 2006 · N269FE · Boeing 727200 · Cargo/Baggage DoorsSDR 06FDEA2220Strap · corrodedBS 950E STR 29 RT IS CORRODED. FOUND CORROSION TO BE ON REPAIR STRAP, REMOVED AND REPLACED REPAIR STRAP BS 950E STR 29R IAW SRM 51-30-2 AND FED EX DWG SR27-53-023 REV A.Jun 6, 2006 · N269FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA2219Repair · damagedEXTERNAL DOUBLER REPAIR 12" X 37" ON LOWER FUSELAGE BETWEEN BS 680-BS 690 STR 26L-27R, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPAIRED DOUBLER AT BS 680 TO BS 720, STR 26L TO SJun 6, 2006 · N269FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2183Repair · misinstalledEXTERNAL REPAIR DOUBLER 22" BY 16" BS 700 STR 27L - 28R IS NOT PER SRM. REMOVED AND REPLACED DOUBLER AT BS 700 STR 27L TO STR 28R IAW SRM 53-30-3.Jun 1, 2006 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2182Repair · misinstalledEXTERNAL REPAIR DOUBLER 11" BY 17" ON LOWER FUSELAGE BS 720 STA 28L -28R IS NOT PER SRM. REMOVED AND REPAIRED DOUBLER BS 720 STR 28L TO 28R IAW SRM 53-30-3.Jun 1, 2006 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2124Shear Tie · corrodedFOUND BS 1110 BETWEEN STRS 30 AND 29 RT SHEAR TIE IS CORRODED. REPAIRED SHEAR TIE IN AFT CARGO BAY AT BS 1110 BETWEEN S30 & 29R IAW SRM 51-40-03.May 31, 2006 · N269FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 06FDEA2058Shear Tie · corrodedFOUND SHEAR TIE AT BS 720, STRINGER 28 LT TO 28 RT CORRODED. REMOVED CORRODED SHEAR TIE AT BS 720 STR 28 RT - 28 LT, FORMED NEW SHEAR TIE AND INSTALLED IAW SRM 53-10-4 AND 51-30-2.May 29, 2006 · N269FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 06FDEA2056Shear Tie · corrodedFOUND SHEAR TIE AT BS 700 STRINGER 28 LT TO 28 RT CORRODED. REMOVED CORRODED SHEAR TIE STR 28 LT - 28 RT BS 700, FORMED NEW SHEAR TIE AND INSTALLED IAW SRM 53-10-4.May 29, 2006 · N269FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 06FDEA2061Doubler · improperEXTERNAL DOUBLER REPAIR 8" BY 14" ON LOWER FUSELAGE BS 1166, STR 19L-20L, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPLACED LOWER FUSELAGE SKIN REPAIR DOUBLER BS 1166 STR 19May 29, 2006 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2060Doubler · improperEXTERNAL DOUBLER REPAIR 7" BY 7" ON LT SIDE OF FUSELAGE AFT OF MLG WHEEL WELL AT BS 950A, STR 25L, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED REPAIR DOUBLER, FABRICATED, DRILLED, TRIMay 29, 2006 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2059Doubler · improperEXTERNAL DOUBLER REPAIR 5" BY 18" ON LOWER FUSELAGE BS 1243, STR 22R, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. INVESTIGATED REPAIR AT BS 1243 STR 22R, FOUND NOT TO BE PER APPROVED DATA. May 29, 2006 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2055Repair · improperEXTERNAL DOUBLER REPAIR 14" BY 16" ON LOWER FUSELAGE CENTERLINE AT BS 660, REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR IS NOT PER SRM, REMOVED EXISTING REPAIR, FABRICATED AND May 29, 2006 · N269FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2057Shear Tie · corrodedFOUND SHEAR TIE AT BS 700 STRINGER 27 LT TO 28 LT CORRODED. REMOVED CORRODED SHEAR TIE STR 27 LT - 28 LT. FORMED NEW SHEAR TIE & INSTALLED IAW SRM 53-10-4.May 29, 2006 · N269FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR 06FDEA2039Stringer · corrodedFOUND STRINGER 28 LT TO BE CORRODED AT BS 680-700. REMOVED S28R AND PRODUCTION SPLICES BS 680-700 AND REINSTALLED NEW STRINGER IAW FED EX SRM 51-30-2.May 26, 2006 · N269FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 06FDEA2038Stringer · corrodedFOUND STRINGER 28 RT TO BE CORRODED AT BS 680-700. REMOVED S28R BS 680-700 RT & PRODUCTION SPLICES AND REINSTALLED NEW STRINGER PER FED EX SRM 51-30-2.May 26, 2006 · N269FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 06FDEA2037Flap Track · corrodedFOUND CORROSION ON NR 6 FLAP TRACK AFT MOUNT PAD. REMOVED AND REPLACED NR 6 FLAP TRACK IAW TASK CARD 27X5708-03.May 26, 2006 · N269FE · Boeing 727233 · Trailing Edge FlapsSDR 06FDEA2028Flap Track · corrodedNR 3 FLAP TRACK UPPER SURFACE CORRODED FWD ATTACH PT OB HOLE. REMOVED AND REPLACED NR 3 FLAP TRACK IAW TASK CARD 27X5705-03.May 26, 2006 · N269FE · Boeing 727233 · Trailing Edge FlapsSDR 06FDEA2029Floorbeam · corrodedFOUND BS 1130 FLOORBEAM TO BE CORRODED AT RBL 7 TO RBL 9 WL 208. REPAIRED BS 1130 FLOOR BEAM RBL 7 - 9 IAW SRM 53-10-8 FIG 11 DETAIL II.May 26, 2006 · N269FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 06FDEA2002Spacer · looseRIGHT ELEVATOR, NR 1 ELEVATOR RUB BLOCK SPACER IS LOOSE IN LOWER TRAILING EDGE BEAM. REPAIRED R/H ELEVATOR NR 1 RUB BLOCK SPACER IN T/E BEAM IAW FED-EX EA 7-5510-100547.May 24, 2006 · N269FE · Boeing 727233 · Elevator StructureSDR 06FDEA1980Shear Tie · corrodedFOUND BS 1148 BETWEEN STRS 30 AND 29 RT SHEAR TIE IS CORRODED. REMOVED SHEAR TIE BS 1148 STR 29 & 30 R/H PER SRM 51-30-2. BLENDED CORROSION 3 X 3 .030. ORIG THICKNESS .063. FOUND TO BE OUT OF LIMITS. FABRICATED NEW SHEAR TIE USING 7075T6 .063 LOT #500810 May 22, 2006 · N269FE · Boeing 727233 · Fuselage Internal Mounting Structure
Back to N269FE, cancelled Aug 22, 2014