Boeing 727-233

Service difficulty reports · 3,034

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = '727233'
  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 06FDEA2648Warning Light · illuminatedMAIN CARGO DOOR "B" LT ILLUMINATED IN FLIGHT, FL250 WITH VENT DOOR WARNING LT IN GALLEY AREA ILLUMINATED.Jul 21, 2006 · N279FE · Boeing 727233 · Door Warning SystemSDR 06FDEA2600Frame · dentedFOUND STA 380 STR 21 RT FRAME INBOARD FLANGE DENTED. REPAIRED DENT AT BS 380 STR 21R IAW SRM 51-40-3.Jul 17, 2006 · N281FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA2599Floorbeam · corrodedFOUND FLOORBEAM AT BS-1110 BL-0 CORRODED ON LOWER FLANGE, UPPER SURFACE. FOUND CORROSION TO BE BEYOND LIMITS, REMOVED DAMAGED SECTION OF FLOORBEAM. FABRICATED REPAIR PARTS, DRILLED, ALODINED, PRIMED REPAIR PARTS AND INSTALLED REF SRM 53-10-1, 51-30-5, 53-10-Jul 17, 2006 · N281FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 06FDEA2598Stringer · crackedFOUND VERTICAL STAB INTERIOR, STR 8L IS CRACKED AT NR 2 RIB. REMOVED DAMAGED AREA OF STR 8L AT NR 2 RIB AND REPAIRED IAW SRM 55-30-4.Jul 17, 2006 · N281FE · Boeing 727233 · Vertical Stabilizer, Spar/RibSDR 06FDEA2601Floorbeam · misdrilledFOUND DOUBLE HOLE IN FLOORBEAM AT BS 910 LBL 65 WL 208 TOP FLANGE FWD SIDES COMMON TO CREASE BEAM WEB. CUT OUT DAMAGED SECTION OF FLOORBEAM AND INSTALLED REPAIR ANGLES ON UPPER CHORD AT BS 910, LBL 65, PER SRM 53-10-8 AND DRAWING NR 06-2756.Jul 17, 2006 · N281FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 06FDEA2496Flap Track · corrodedFOUND CORROSION ON NUMBER 3 FLAP TRACK AFT MOUNTING SURFACE. REMOVED AND REPLACED #3 FLAP TRACK IAW FED EX WORK CARD 27X5705-03Jul 10, 2006 · N281FE · Boeing 727233 · Trailing Edge FlapsSDR 06FDEA2494Shear Plate · misdrilledFOUND VERT FIN, LT UPPER SHEAR PLATE TO HAVE 3 "SNOWMAN" HOLES. REMOVED AND REPLACED VERT FIN LT UPPER SHEAR PLATE IAW SRM 51-30-2, 51-30-5Jul 10, 2006 · N281FE · Boeing 727233 · Vertical StabilizerSDR 06FDEA2493Fitting · damagedFOUND VERT FIN "C" SHAPED SHEAR FITTING TO HAVE 3 "SNOWMAN" HOLES. REMOVED AND REPLACED VERT FIN "C" SHAPED SHEAR FITTING IAW SRM 51-30-2, 51-30-5Jul 10, 2006 · N281FE · Boeing 727233 · Vertical Stabilizer, Attach FittingsSDR 06FDEA2499Skin · damagedFOUND FUSELAGE SKIN UNDER ATC NR 2 ANTENNA, HAS SCRIBE MARKS. REMOVED DAMAGE FROM FUSELAGE SKIN UNDER ATC NR 2 ANTENNA REPAIRED IAW SRM 53-30-3Jul 10, 2006 · N281FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2498Skin · misrepairedFOUND FLUSH DOUBLER REPAIR STA 680-688 STR 28R - 29R, REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. PREVIOUSLY INSTALLED REPAIR BS 680-688 STR 28-29R DID NOT COMPLY WITH APPROVED FAA REPJul 10, 2006 · N281FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2497Skin · crackedFOUND LEFT WING T/E I/B MIDFLAP, CRACKED AT CUTOUT FOR INBOARD PUSHROD IN AFT CHORD. REPAIRED CRACK ON LEFT WING T/E IB MIDFLAP IAW SRM 51-30-2, 51-40-4 FIG 1Jul 10, 2006 · N281FE · Boeing 727233 · Trailing Edge FlapsSDR 06FDEA2495Beam · chafedMAIN CARGO BAY, LONGITUDINAL BEAM IS CHAFED AT FASTENER HOLES (FROM NUTPLATES) BS 850 TO BS 763 RBL 25 WL 208. FOUND CHAFE AREA TO BE BEYOND LIMITS. REMOVED TRACK EXPANSION LINK AND LONGITUDINAL BEAM, RBL 25, LOCATED AND DRILLED NEW LONGITUDINAL BEAM. INSJul 10, 2006 · N281FE · Boeing 727233 · Fuselage Main, StructureSDR PCSA7090601Fuel Tank · leakingDURING THE MAINTENANCE WALK AROUND INSPECTION, A FUEL LEAK WAS DISCOVERED AT THE REAR SPAR OF THE NR 2 FUEL TANK (WING BOX CENTER SECTION). FURTHER INSPECTION REVELED CORROSION BEYOND LIMITS IN THE NR 2 FUEL TANK AT THE REAR SPAR. REPAIR WEB DOUBLER AND STIFJul 9, 2006 · N395AJ · Boeing 727233 · Fuel StorageSDR 06FDEA2471Carriage · gougedFOUND RT WING I/B AFT FLAP, I/B CARRIAGE GOUGED. REPAIR ACCOMPLISHED PER FED EX EA 7-5710-100554.Jul 7, 2006 · N281FE · Boeing 727233 · Trailing Edge FlapsSDR 06FDEA2454Beam · chafedMAIN CARGO BAY LONGITUDINAL BEAM IS CHAFED AT FASTENER HOLES FROM NUTPLATES BS 850 TO BS 763 RBL 45 WLO 208. REMOVED DAMAGED LONGITUDINAL BEAM AND REPLACED WITH NEW LONGITUDINAL BEAM ALL WORK DONE IAW SRM 51-30-2.Jul 3, 2006 · N281FE · Boeing 727233 · Fuselage Main, StructureSDR 06FDEA2453Stringer · chafedFOUND FWD CARGO BAY, CHAFED STRINGER BS 560 LT AT STRINGER 21. REPAIRED STRINGER 21L FROM BS 533 TO BS 566 IAW SRM 53-10-3.Jul 3, 2006 · N281FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 06FDEA2452Stringer · chafedFOUND FWD CARGO BAY, CHAFED STRINGER BS 540 LT AT STRINGER 21. REPAIRED STRINGER 21L FROM BS 560 TO BS 566 IAW SRM 53-10-3.Jul 3, 2006 · N281FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 06FDEA2451Frame · chafedFOUND UPPER INTERIOR, STA 520, FRAME IS CHAFED AT SIDEWALL PANEL SUPPORT STR 11 RT. REPAIRED FRAME STA 520 AT STR 11R IAW SRM 51-40-3Jul 3, 2006 · N281FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA2450Frame · chafedFOUND UPPER LOBE INTERIOR, STA 540, FRAME IS CHAFED AT SIDEWALL PANEL SUPPORT STR 11 RT. REPAIRED STA 540 FRAME IAW SRM 51-40-3 STR 11 RT.Jul 3, 2006 · N281FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA2449Frame · chafedFOUND UPPER LOBE INTERIOR, STA 500, FRAME IS CHAFED AT SIDE WALL PANEL SUPPORT STR 11 RT. REPAIRED FRAME STA 500 AT STR 11R IAW SRM 51-40-3.Jul 3, 2006 · N281FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA2448Frame · chafedFOUND UPPER LOBE INTERIOR, STA 480, FRAME IS CHAFED AT SIDEWALL PANEL SUPPORT STR 11 RT. REMOVED AND REPAIRED DAMAGE STA 480 FRAME STR 11 RT IAW SRM 53-10-1Jul 3, 2006 · N281FE · Boeing 727233 · Fuselage Main, FrameSDR 06FDEA2447Pressure Panel · corrodedFOUND LT WHEEL WELL PRESSURE WEB CORRODED B/S 886, LBL 45 WL 202. BLENDED CORROSION FROM LT WW PRESSURE WEB 1"X1" 100% MAT. THICKNESS OUT OF LIMITS PER 51-30-1. REMOVED WEB AND FABRICATED NEW WEB FROM 2024-T30.032" LOT #664145 AND INSTALLED ALL IAW SRM 51Jul 3, 2006 · N281FE · Boeing 727233 · Fuselage Main, BulkheadSDR 06FDEA2446Spar · chafedFOUND VERTICAL STAB LT MID SPAR CHORD FIN STA 225.71 CHAFED.Jul 3, 2006 · N281FE · Boeing 727233 · Vertical Stabilizer, Spar/RibSDR PCSA062206SUPBlades · damagedON TAKEOFF CREW REPORTED NR 1 BLEED TRIP LIGHT CAME ON. CHANGED TO NR 2 BLEED, ONE MIN LATER NR 1 STRUT OVERHEAT LIGHT CAME ON. FOLLOWED COMPANY CHECKLIST & SHUT DOWN NR 1 ENGINE; DUMPED FUEL, & RETURNED WITHOUT INCIDENT. INSPECTION OF NR 1 ENGINE FOUND C-Jun 22, 2006 · N495AJ · Boeing 727233 · Turbine Engine Compressor SectionSDR PCSA06220601Warning System · multiple failFLIGHT 611 ON TAKEOFF FROM MIA THE CREW REPORTED THE NR 1 BLEED TRIP LIGHT CAME ON. THE CREW THEN CHANGED TO THE NR 2 BLEED, ONE MINUTE LATER THE NR 1 STRUT OVERHEAT LIGHT CAME ON. THE CREW FOLLOWED THE COMPANY CHECKLIST AND SHUT DOWN THE NR 1 ENGINE; DUMPEDJun 22, 2006 · N495AJ · Boeing 727233 · Central WarningSDR 06FDEA2367Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 500, STR 29L IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER IAW SRM 53-30-3, FIGURE 3 AND REINSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3 AND SRM 51-30-2. REPAIR IS CLASSIFJun 19, 2006 · N257FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR PCSA06080601Hinge Bracket · corrodedDURING PUSHBACK MAINTENANCE FOUND THE RT AFT OVERWING EXIT STEP MISSING. ON FURTHER INSPECTION MAINTENANCE FOUND CORROSION ON THE RT AFT OVERWING EXIT STEP HINGE HALF, AMERIJET MAINTENANCE INSPECTED THE RIGHT HAND FUSELAGE, THE RIGHT HAND WING AND THE VERTICAJun 8, 2006 · N495AJ · Boeing 727233 · Emergency ExitsSDR CA060608001Switch · malfunctionedAFTER DEPARTURE ON AN ACCEPTANCE FLIGHT AFTER HEAVY MAINTENANCE, THE CREW OBSERVED A NR 1 CARGO DOOR UNSAFE INDICATION. THE WARNING LIGHT EXTINGUISHED AT 7.2 PSID AFTER REDUCING ALTITUDE TO 11K FT. THE AIRCRAFT RETURNED TO POINT OF DEPARTURE WHERE THE SWITCHJun 4, 2006 · Boeing 727233 · Door Warning SystemSDR 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 06FDEA2144Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED AT STA 188 BELOW STR 24L IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER IAW SRM 53-30-3 FIG 3 AND REINSTALLED REPAIR PARTS PER SRM 51-10-2 AND MM 51-20-151-7. REPAIR IS CLASSIFIED AMay 31, 2006 · N276FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 06FDEA2143Repair · improperFOUND PREVIOUSLY REPAIR LOCATED AT STA 990 STR 24R IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED REPAIR PART DOUBLER IAW SRM 53-30-3 FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 53-30-3 FIG 1 AND SRM 51-30-2. REPAIR IS CLASSIFIED AS May 31, 2006 · N276FE · 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 06FDEA2095Skin · misrepairedFOUND PREVIOUSLY REPAIR LOCATED AT NR 3 CARGO DOOR EXTERNAL SKIN UPPER AFT EDGE IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED REPAIR PARTS IAW SRM 52-00-3 FIG 3. INSTALLED REPAIR PART IAW SRM 52-00-3, FIG 3. REPAIR IS CLASSIFIEDMay 31, 2006 · N276FE · Boeing 727233 · Cargo/Baggage DoorsSDR 06FDEA2081None · noneFOUND PREVIOUSLY REPAIR INSTALLED FROM STA 970-990, STR 29R WAS DETERMINED TO BE ACCOMPLISHED PER BOEING SB 727-53-0179, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENERS SPACING AND NUMBERS, GENEMay 30, 2006 · N276FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA2080None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 950D, STR 18R WAS DETERMINED TO BE ACCOMPLISHED IAW FEDEX EA 5310-57265, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMay 30, 2006 · N276FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA2079None · noneFOUND PREVIOUSLY REPAIR INSTALLED BETWEEN STA 950-950C, STR 29L WAS DETERMINED TO BE ACCOMPLISHED IAW FEDEX EA 5380-55160, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENERS SPACING AND NUMBERS, GEMay 30, 2006 · N276FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA2078None · noneFOUND PREVIOUSLY REPAIR DOUBLER/TRIPLER INSTALLED AT STA 1090 FWD LOWER SIDE OF AFT CARGO DOOR CUT OUT WAS DETERMINED TO BE ACCOMPLISHED IAW EA 7-5330-55172 BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS,May 30, 2006 · N276FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA2077None · noneFOUND PREVIOUSLY REPAIR LOCATED AT STA 178, FWD SIDE OF BULKHEAD, LT BOTTOM WAS DETERMINED TO BE ACCOMPLISHED PER SRM 53-10-9, FIG 3, BASED ON AN EXTERNAL EVALUATION, CONSIST OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS,May 30, 2006 · N276FE · Boeing 727233 · Standard Practices/StructuresSDR 06FDEA2076None · noneFOUND PREVIOUSLY REPAIR INSTALLED AT STA 196.5, STR 24R WAS DETERMINED TO BE ACCOMPLISHED IAW SRM 53-30-3 FIG. 6, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS AND GENERAL WMay 30, 2006 · N276FE · Boeing 727233 · Standard Practices/StructuresSDR 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 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 Beam
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