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 98FDEA00210Spar Web · crackedNR 0901, RT AILERON, OUTBOARD HAS CRACK IN SPAR WEB AT FASTENER HOLE. THIS REPAIR TIED TO REPAIR BEING PERFORMED ON NR0324. STOP DRILLED CRACK AND FABRICATED DOUBLER AND INSTALLED REPAIR PER EA 7-5750-29411.Mar 18, 1998 · N268FE · Boeing 727233 · AileronsSDR CA971216069Fire Loop · intermittant(CAN) ON DEPARTURE AT FL 200, CREW OBSERVED FIRE WARNING. NR 1 ENG SHUT DOWN AND A/C RETURNED. UNABLE TO DETECT FAULT. TWO FIRE LOOPS AND CONTROL UNIT RELACED.Mar 17, 1998 · Boeing 727233 · Fire DetectionSDR AALA980514Light · defectiveDFW - DURING OVERNIGHT CHECK, AFT STAIRWAY EMERGENCY LIGHT ASSEMBLY WAS INOPERATIVE. REPLACED AFT STAIRWAY EMERGENCY LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Mar 17, 1998 · N866AA · Boeing 727233 · Emergency LightingSDR 98FDEA00200Engine · fodON CLIMBOUT AT ABOUT 4500 FT MSL (3000' AG) A LARGE BIRD FLEW RIGHT OVER COCKPIT AND INTO NR 2 ENGINE. AIRCRAFT HAD BAD VIBRATION, EVEN AT IDLE, SHUTDOWN NR 2 ENGINE. EGT DID NOT EXCEED LIMITS. NUMBER 2 ENGINE REPLACED PER FEDEX B727 ENGINE REPLACEMENT WORKMar 13, 1998 · N222FE · Boeing 727233 · Engine (Turbine/Turboprop)SDR 98FDEA00213Light · rustedNR 0407, FWD ENTRY DOOR SLIDE LIGHT HAS LENS SCREWS NUT PLATES RUSTED OFF. REMOVED AND INSTALLED SERVICEABLE SLIDE LIGHT ASSY NR 33960.Mar 12, 1998 · N268FE · Boeing 727233 · Emergency LightingSDR 98FDEA00196Stringer · crackedNR 0578 AFT OF BS 720B, R STR 15, AT LEADING EDGE LIGHT CRACKED. REPAIRED STRINGER, CUT OUT DAMAGED AREA INSTALLED U CHANNEL AND FILLER PER SRM 53-10-5 FIG 5.Mar 12, 1998 · N263FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 98FDEA00195Stringer · corrodedNR 0591, FWD CARGO, STRINGER CORRODED UNDER STAND, OFF NUTPLATE BS 550 L AT STRINGER 27L. REMOVED DAMAGED AREA OF STRINGER PER SRM 53-10-3 FIG 1 SHEET 1. MADE DOUBLER AND FILLER FROM BAC1498-108 AND BAC1498-133 MATERIAL PER SRM 53-10-3 FIG 1 SHEET 2. ALODINMar 12, 1998 · N263FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 98FDEA00194Frame · dentedNR 0775, FWD LOWER CARGO COMPT, FRAME DENTED BS 600 AT STR 24 - 25 LT. REMOVED DAMAGED AREA, FABRICATED, ALODINED AND PRIMED REPAIR DOUBLER AND INSTALLED DOUBLER PER SRM 53-10-4 FIGURE 1 (SHEET 3).Mar 12, 1998 · N263FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00193Frame · dentedNR 0917, FWD LOWER CARGO COMPT: FRAME DENTED AT BS 520, STR 23 - 24 RT. REMOVED DAMAGED FRAME SECTION LOWER FORWARD CARGO BS 520, STR 23 - 24 RT. INSTALLED DOUBLER AND NEW STRINGER CLIPS PER SRM 51-40-3 FIG 1 (SHEET 4) AND SRM 51-10-1.Mar 12, 1998 · N263FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00192Frame · dentedNR 0259, FWD CARGO BELT FRAME DENTED AT BS 580 BETWEEN STRS 23 - 25 L. REMOVED DAMAGE. INSTALLED DOUBLER BS 580 BETWEEN STRS 23 - 25 L PER SRM 51-40-3.Mar 12, 1998 · N268FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00191Frame · dentedNR 0260, FWD CARGO, BELT FRAME DENTED AT BS 560 BETWEEN STRS 22 - 25 L. REMOVED DAMAGE. INSTALLED REPAIR DOUBLER ON BELT FRAME PER SRM 51-40-3.Mar 12, 1998 · N268FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00190Skin · crackedNR 0271 7-5330-7-2345 P1-3, SKIN CRACKED AT LOWER HINGE AT FWD ENTRY DOOR. ROUTED OUT CRACK. VERIFIED BY NDT. INSTALLED DOUBLER PER EO 7-5330-7-2345 C2.Mar 12, 1998 · N268FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 98FDEA00189Frame · dentedNR 0268 FWD CARGO, BELT FRAME DENTED ( 2 PLACES ) AT BS 500 BETWEEN STRS 22 - 24 L. REMOVED DAMAGE. INSTALLED DOUBLER AT BS 500 BETWEEN STRS 22 - 24 L PER SRM 51-40-3.Mar 12, 1998 · N268FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00188Frame · dentedNR 0267 FWD CARGO, BELT FRAME DENTED (2 PLACES) AT BS 520 BETWEEN STRS 23 - 25 L. REMOVED DAMAGE. INSTALLED REPAIR DOUBLER ON BELT FRAME PER SRM 51-40-3.Mar 12, 1998 · N268FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00187Stringer · crackedNR 0263 71C203-02 FWD CARGO BS 560, STR 24 LT, STRINGER CRACKED UPPER FLANGE. STOP DRILLED CRACK PER SRM 51-10-1. ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED DOUBLER PER SRM 53-10-3.Mar 12, 1998 · N268FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 98FDEA00186Rib · damagedNR 0905 RT OUTBD AILERON HAS .25 DIA CHERRY MAX FASTENER IN UPPER SKIN, RIB IS .600 WIDE, ORIGINAL FASTENERS WERE .125 DIA COUNTER SINK INTO RIB WILL HAVE DAMAGED RIB AND MINIMUM ED IS LOST IN RIB. REMOVED AND REPLACED RIB PER SRM 51-10-1. SKIN REPAIR ACCOMPMar 12, 1998 · N268FE · Boeing 727233 · AileronsSDR 98FDEA00185Frame · dentedNR 0253 FWD CARGO, BELT FRAME DENTED BS 700, STR 22 R. REMOVED DAMAGE. INSTALLED DOUBLER PER SRM 51-40-3.Mar 12, 1998 · N268FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00184Frame · dentedNR 0257 FWD CARGO, BELT FRAME DENTED ( 2 PLACES) BS 680, AT STR 23 AND STR 22 R. REMOVED DAMAGE, INSTALLED DOUBLER PER SRM 51-40-3.Mar 12, 1998 · N268FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00183Frame · dentedNR 0256 FWD CARGO, BELT FRAME DENTED BS 680, STR 25 R. REMOVED DAMAGE. FABRICATED AND DRILLED DOUBLER AND PRIMED ALL BARE METAL. INSTALLED DOUBLER PER SRM 51-40-3.Mar 12, 1998 · N268FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00182Frame · dentedNR 0258 FWD CARGO, BELT FRAME DENTED BS 700, STR 24 R. REMOVED DAMAGE. INSTALLED DOUBLER PER SRM 51-40-3.Mar 12, 1998 · N268FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00178Frame · dentedFWD CARGO, BS 700, STR 23 TO 24 RT BELL FRAME DENTED. CUT OUT DAMAGED AREA OF BELL FRAME PER SRM 53-10-7 PAGE 1. ALODINED AND PRIMED PER M/M 51-20-0. INSTALLED BELL FRAME REPAIR PER SRM 51-40-3 FIG 1.Mar 12, 1998 · N263FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00177Skin · gougedFWD CARGO AFTER REMOVAL OF INTERCOSTAL (PER CARD 7-5330-7-2352 P2 SECTION B/2) SKIN INNER SURFACE, WAS FOUND TO BE GOUGED IN SEVERAL AREAS BS 700 TO 720 O/B OF STR 28L. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLER PER SRM 53-30-3.Mar 12, 1998 · N263FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 98FDEA00176Frame · dentedFWD CARGO BS 700, STR 23 TO 24 LT BELL FRAME DENTED. REMOVED DAMAGED AREA OF BELL FRAME PER SRM 51-40-3. ALODINED AND PRIMED PER M/M 51-20-0. INSTALLED DOUBLER PER SRM 51-40-3.Mar 12, 1998 · N263FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00175Frame · damagedUPPER LOBE BS 1130, BETWEEN STR 13L AND 14L BELL FRAME HAS DAMAGED AREA AND BARE METAL. REMOVED DAMAGED AREA OF BELL FRAME. ACCOMPLISHED BELL FRAME REPAIR PER SRM 53-10-4 PG 7-11.Mar 12, 1998 · N263FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00174Frame · dentedFWD LWR CARGO FRAME DENTED BS 560, STR 24L TO 25L. REMOVED DAMAGE, INSTALLED BELTFRAME DOUBLER REPAIR PER SRM 51-40-3.Mar 12, 1998 · N263FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00179Frame · dentedFWD LWR CARGO FRAME DENTED BS 660, STR 22 TO STR 23. REMOVED DAMAGE FROM FRAME, PREPARED DOUBLER, ALODINED, PRIMED AND INSTALLED DOUBLER PER SRM 53-10-4.Mar 11, 1998 · N263FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00153Actuator · failed98-0058 AFTER TAKEOFF WITH GEAR AND FLAPS UP, LEADING EDGE DEVICE INDICATIONS WERE NORMAL. SYSTEM 'A' LOST ALL QUANTITY. DURING HYDRAULIC LOSS CHECK LIST, LEADING EDGE DEVICE MALFUNCTION, LIGHT ON SLAT NR 8 WAS AMBER. AFTER AIRCRAFT TOW IN, FOUND NR 8 SLAT Mar 5, 1998 · N219FE · Boeing 727233 · Leading Edge Slat ActuatorSDR 98FDEA00149Skin · crackedRT WING NR 8 L/E SLAT, LOWER SKIN TANG BELOW INBD TRACK ATTACH CRACKED AND RIVETS PULLED. ACCOMPLISHED REPAIR ON RT WING NR 8 L/E SLAT FOR CRACKED LWR SKIN TANG BELOW INBOARD TRACK PER AA 7-5750-29381 AND AA SRM 57-50-1 PGS 7A AND 7B.Feb 25, 1998 · N271FE · Boeing 727233 · Leading Edge DevicesSDR 98FDEA00139Switch · out of adjustTAIL SKID LIGHT ILLUMINATES WHEN GEAR IS PLACED TO DOWN AND LOCKED POSITION IN THE AIR. GEAR WAS RECYCLED AND LIGHT REMAINS ON. ADJUSTED AND CLEANED THE TAIL SKID WARNING LIGHT SWITCH, (DOWN LOCK), PER MAINTENANCE MANUAL 32-71-01. GROUND CHECK OK.Feb 25, 1998 · N218FE · Boeing 727233 · Landing Gear Position and WarningSDR 98FDEA00136Fire Detector · failedAUXILIARY POWER UNIT FIRE WARNING LIGHT (NO AURAL) AND GLARESHIELD LIGHT ILLUMINATED AT FLIGHT LEVEL 310 0+30 MINUTES. AUXILIARY POWER UNIT FIRE HANDLE PULLED AND DISCHARGED AUXILIARY POWER UNIT FIRE BOTTLE. *S/D* FOUND RECTIFIER/DIODE ASSY RACK RECEPTACLE EFeb 24, 1998 · N278FE · Boeing 727233 · Fire DetectionSDR 98FDEA00125Engine · bird strikeMULTIPLE BIRD STRIKE AT 1300 FT, FLAPS 5 DEGREES. NR 1 ENGINE WAS SHUT DOWN FOR VIBRATION AND SUBSEQUENT FAILURE. REMOVED AND REPLACED NR 1 ENGINE ASSEMBLY PER WORK CARD 70T0001 AND OPERATIONAL CHECKS GOOD. NO LEAKS NOTED ON RUN CHECK. REFERENCE WORK CARD 7Feb 24, 1998 · N270FE · Boeing 727233 · Engine (Turbine/Turboprop)SDR 98FDEA00128Frame · damagedLOWER LOBE AFT CARGO BS 1130 FRAME DAMAGED BELOW LT EDGE SUPPORT PANEL ON TOP ANGLE BETWEEN STR 27L TO 28L. INSTALLED DOUBLER PER SRM 53-10-4.Feb 23, 1998 · N271FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00127Stiffener · crackedLOWER LOBE AFT CARGO, BS 1183 BULKHEAD LOWER END OF VERTICAL STIFFENER AT RBL 8.0 CRACKED IN I/B RADIUS (INITIAL CRACK LENGTH 1.875.). INSTALLED RBL 8 VERTICAL BEAM MODIFICATION AND REPAIR PER S/B 53-175R2, AD 90-06-09 AND DRAWING 65C29080 GN7.Feb 23, 1998 · N271FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00126Frame · damagedLOWER LOBE AFT CARGO BS 1110 FRAME DAMAGED BELOW LT EDGE SUPPORT PNL, ON TOP ANGLE, BETWEEN STR 27L TO 28L. REMOVED DAMAGED AND INSTALLED DOUBLER PER SRM 53-10-4.Feb 23, 1998 · N271FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00124Chord · corrodedCORROSION BS 1070, WL 201, LBL 45 - RBL 45 ON LOWER CHORD. *S/D* REPAIRED LOWER CHORD BS 1070, WL 201, LBL 45 - RBL 45 IAW FED-EX EA NR 7-5310-37461.Feb 23, 1998 · N222FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00119Fire Loop · malfunctionNR 3 FIRE LIGHT ILLUMINATED WITH BELL AT FL 290. AFTER SWITCHING ESSENTIAL POWER, LIGHT AND BELL WENT OUT NEVER TO COME ON AGAIN. NEVER ANY INDICATION OF FIRE VISUALLY INSPECTED NR 3 ENGINE AND FIRE LOOP. LOOKED GOOD, OPS CHECKED GOOD.Feb 19, 1998 · N220FE · Boeing 727233 · Fire DetectionSDR 98FDEA00129Skin · gougedUPPER LOBE, FUSE CROWN SKIN GOUGED AT BS 1050 BETWEEN STRINGER 3L TO 4L. TRIMMED OUT DAMAGED AREA. INSTALLED EXTERNAL REPAIR DOUBLER PER SRM 53-30-3.Feb 13, 1998 · N271FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 98FDEA00105Chord · corrodedNR 0025 006 CORROSION ON LOWER CHORD BS 1130, WL 201, LBL 25 TO RBL 25. REPAIRED LOWER CHORD AT BS 1130, WL 201, LBL 62 TO RBL 62. ALL WORK DONE IAW FED-EX EA NR 7-5310-37462.Feb 12, 1998 · N222FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00104Chord · corrodedCORROSION FOUND ON LOWER CHORD AT BS 1148, LBL 30 TO RBL 43, WL 201 FLOORBEAM. *S/D* REMOVED CORROSION BS 1148, LBL 30 TO RBL 43, WL 201. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-01. FABRICATED REPAIR PARTS, ALODINED AND PRIMED PARTS. INSTALLED ALL Feb 12, 1998 · N222FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00098Chord · corrodedNR 0021 002, CORROSION LOWER CHORD BS 1050, WL 201, RBL 15. REMOVED DAMAGED AREA BS 1050, WL 201, RBL 13. FABRICATED REPAIR PARTS, ALODINED AND PRIMED. INSTALLED REPAIR PARTS PER FED-EX SRM 53-10-08 FIG 8.Feb 11, 1998 · N222FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00097Stringer · crackedNR 0029 003 WHILE WORKING 7-5450-7-3301L PT 11 FOUND CRACK IN STRINGER 14L AT BS 1243. REPAIRED STR 14L, BS 1233 TO BS 1253 IAW FED-EX SRM 53-10-3, 53-10-4.Feb 11, 1998 · N222FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 98FDEA00096Chord · corrodedCORROSION UPPER CHORD BS 1030, WL 208, LBL 11 TO 21. *S/D* REMOVED CORROSION BS 1030, WL 208, LBL 11 TO 21. FOUND TO BE IN LIMITS PER FED-EX SRM 53-10-01. ALODINED AND PRIMED ALL EFFECTED AREA.Feb 11, 1998 · N222FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00091Floorbeam · corrodedNR 0023 001, CORROSION LOWER CHORD BS 1010, WL 201, LBL 24 TO 36. REMOVED CORROSION ON LOWER CHORD, BS 1010, WL 201, LBL 1 TO 45.5. REMOVED LOWER FLANGE OF LOWER CHORD. FABRICATED REPAIR PARTS AND INSTALLED IAW FED-EX SRM 53-10-8 FIG 2.Feb 10, 1998 · N222FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 98FDEA00103Floorbeam · damagedNR 0752, NR 0754, UPPER LOBE, BS 420, FLOORBEAM HAS DRILL MARK ALMOST THROUGH UPPER LIP AT RBL 6. ADDITIONAL DAMAGE FOUND IN FLOORBEAM AT RBL 3 UPON REMOVAL OF SEAT TRACK. REMOVED DAMAGED AREAS OF FLOORBEAM AT RBL 3 AND RBL 6, BS 420, AND REPAIRED PER SRM 53Feb 6, 1998 · N264FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 98FDEA00102Stringer · crackedNR 0221 BS 720B PLUS 5, STRINGER 15R END CRACKED AT HI-LOK FWD OF WING SCANNING LIGHT. CUT END OF STR HFEC CHECKED CUT EDGE OF STRINGER. FABRICATED U-CHANNEL OF .040 7075-T6 AND FILLERS. INSTALLED REPAIR IAW SRM 53-10-3 FIG 5.Feb 6, 1998 · N264FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 98FDEA00063Floorbeam · corrodedNR 0727 72 C235-02 UPPER LOBE, BS 344, LBL 60 - RBL 20. CORROSION ON FLOORBEAM UPPER CAP. REMOVED OLD UPPER FLOORBEAM T-CAP. INSTALLED NEW T-CAP FROM LT TO RT SIDE OF FUSELAGE PER SRM 53-10-8 AND SRM 27-53-007, SHEET 1 OF 1.Jan 29, 1998 · N264FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 98FDEA00062Floorbeam · corrodedNR 0683 AND NR 1044 72 C237-02 UPPER LOBE BS 1070, RBL 20 - RBL 35, CORROSION ON TOP SIDE OF FLOORBEAM. CUTOUT 2 AREAS OF CORROSION ON FLOORBEAM T CAP. INSTALLED REPAIR FROM RBL 16 - RBL 54, PER SRM 53-10-8, FIG 1.Jan 29, 1998 · N264FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 98FDEA00061Floorbeam · corrodedNR 1051 72 C237 02 UPPER LOBE BS 1050, RBL 20 CORROSION ON TOP LEG OF FLOORBEAM. REMOVED CORROSION CUTOUT DAMAGED AREA. FABRICATED REPAIR PARTS. INSTALLED REPAIR PER SRM 53-10-8 FIG 1.Jan 29, 1998 · N264FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 98FDEA00073Stringer · crackedFWD CARGO STRINGER 26L CRACKED AT BS 520. REMOVED DAMAGED AREA OF STRINGER AND SPICED IN NEW SECTION PER SRM 53-10-3 PAGE 4B.Jan 27, 1998 · N264FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 98FDEA00066Web · crackedNR 0141 BS 913.5 LEFT MAIN WHEEL WELL HAS CRACK ABOVE FILLER OF FLANGE. CONFIRMED WITH HFEC IN NOTED AREA. STOP DRILLED CRACK PER SRM 51-10-1 AND INSTALLED MODIFICATION KIT P/N 5561732 (ON ORDER FORM NR 43326) IN ACCORDANCE WITH BOEING 727 SRM 53-10-2 PAGE 2Jan 27, 1998 · N264FE · Boeing 727233 · Fuselage Miscellaneous Structure
Back to Boeing 727-233