Boeing 727-233

Service difficulty reports · 3,034

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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 98FDEA00449Line · malfunctionSTA-IND - NR 1 ENGINE LOST OIL QUANTITY APPROXIMATELY 5 MINUTES LATER OIL PRESSURE STARTED TO DROP. ENGINE SHUT DOWN PER RED TABS. OIL PRESSURE NEVER AT 0 PSI. WINDMILLED WITH OIL PRESS AT 20 PSI FOR 20 MINUTES. REMOVED AND REPLACED OIL LINE TO #6 BEARING,Jul 10, 1998 · N267FE · Boeing 727233 · Turbine Engine Oil SystemSDR 98FDEA00417Switch · failed98-0160 STA-IND: AFTER TAKEOFF AND INITIAL CLEAN UP, PASSING THROUGH 10,000 FEET FROM THE ACCELERATION TO CLIMB SPEED, THE FRONT AMBER LEADING EDGE WARNING CAME ON. PER POSITION INDICATION SHOWED THE NR 4 LEADING EDGE DEVICE AS CONSTANTLY YELLOW IN TRANSIT. Jun 26, 1998 · N270FE · Boeing 727233 · Leading Edge Slat Control SystemSDR 98FDEA00414Fire Warning · malfunction98-0157 STA-DAY - MASTER FIRE WARNING LIGHTS AND BELL ANNUNCIATED WITH NO OTHER INDICATIONS. WARNING SYSTEMS CHECKED OK ON ENGINE, SMOKE, AND APU, NO FAULTS. 10,000 FEET 300 KTS. COULD NOT DUPLICATE ENGINE, APU AND SMOKE DETECTION SYSTEM CHECKS GOOD ON GROJun 23, 1998 · N280FE · Boeing 727233 · Fire DetectionSDR 98FDEA00377Clamp · loose98-0145, NUMBER 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT WITH WING ANTI-ICE OFF, LIGHT WENT OUT WHEN THROTTLE WAS RETARDED. RAN ENGINE FOUND CLAMP ON DUCT COMING FROM THE PRECOOLER LEAKING. TIGHTENED CLAMP, RAN ENGINE AGAIN LEAK CHECKED GOOD. OPEMay 27, 1998 · N265FE · Boeing 727233 · Pneumatic Distribution SystemSDR 98FDEA00354Actuator · failedAFTER T/O, DURING FLAP RETRACTION FROM 2 DEG TO UP, AMBER LEADING FLAPS LIGHT REMAINED ON, NR 3 SLAT AMBER LIGHT IND INTERMEDIATE POS, A-SYS HYD QTY OBSERVED AT ZERO. RED TAB CKLT ACCOMPLISHED. SAFETY WIRE BROKEN ON A FLUID S/O VALVES AND GPWS FLAP. UNEVENTMay 19, 1998 · N280FE · Boeing 727233 · Leading Edge Slat ActuatorSDR 98FDEA00339Engine · failedON T/O, NR 3 ENG FAILED, SLIGHT SHUDDER ACCOMMP BY LOSS OF EPR AND N1, HIGH EGT AND LOSS OF OIL QTY, SHUTDOWN PER 727 A/C FLT MANUAL. REMOVED AND REPLACED NR 3 ENG PER W/C 70T0001.May 12, 1998 · N258FE · Boeing 727233 · Engine (Turbine/Turboprop)SDR 98FDEA00334Overheat Loop · out of positionLOWER AFT BODY OVERHEAT LIGHT CAME ON IN FLIGHT WITH WING ANTI-ICE ON. TURNED OFF WING ANTI-ICE, LIGHT WENT OUT. TURNED ENGINE NR 1 WING ANTI-ICE ON LIGHT CAME BACK ON. SECURED SYSTEM THEN RECHECKED WITH ENGINE NR 3 WING ANTI-ICE ON, LIGHT CAME BACK ON AGAIMay 6, 1998 · N274FE · Boeing 727233 · Overheat DetectionSDR 98FDEA00323Crease Beam · corrodedCORROSION (C53-224-01) ON CREASE BEAM AROUND FASTENER HOLES ON UNDERSIDE AT BS 304 TO 358, LBL 60, WL 208. *S/D* REMOVED AND REPLACED CREASE BEAM BS 294 TO 360, LBL 60, WL 208 IAW FED-EX SRM 51-30-2. PAINTED IAW FED-EX M/M 51-20-151.May 1, 1998 · N265FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00321Clip · corrodedSTRINGER 26R CLIP AT BS 698 CORRODED. *S/D* FOUND STRINGER CLIP AT BS 698, STR 26R TO BE OUT OF LIMITS. INSTALLED NEW STR CLIP IAW FED-EX SRM 53-10-1 AND SRM 51-30-2.May 1, 1998 · N265FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00320Shutoff Valve · inoperativeREPEAT WRITE-UP FROM DISCREPANCY NR 01199454 ENGINE NR 3 STRUT OVERHEAT LIGHT ON. OVERHEAT LIGHT CAME ON PASSING FLIGHT LEVEL 250 AND APPROXIMATELY 20 MINUTES INTO FLIGHT. BOTH PACKS ON NR 1 BLEED OFF, NR 2 OPEN NR 3 OPEN CLIMB POWER WITHIN PARAMETERS. ADMIApr 30, 1998 · N222FE · Boeing 727233 · Pneumatic Distribution SystemSDR 98FDEA00313Stringer · damgedNR 1028, HOLE IN RADIUS OF STR 25L, BS 520 IN LWR FWD CARGO. CUT OUT DAMAGE AND INSTALLED 2 SPLICE REPAIRS PER 53-10-3.Apr 28, 1998 · N267FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 98FDEA00312Floorbeam · corrodedNR 0891, 72-C235-02, BS 344 FLOORBEAM LBL 60 TO RBL 25 HAS CORROSION AROUND NUTCLIP HOLES. INSTALLED REPAIR STRAPS IAW SRM 53-10-07-2 P 1-3.Apr 28, 1998 · N267FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 98FDEA00310Stringer · crackedNR 0200, 72-C235-02, MAIN CARGO - 2 CRACKS TO STR 15R, BS 720B + 6 JUST FWD OF WING LIGHTS. REPAIRED STRINGER AT WING SCANNING LIGHT PER SRM 53-10-3 FIG 5.Apr 28, 1998 · N267FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 98FDEA00299Shear Tie · corrodedWHILE WORKING NR0450 FOUND SHEAR TIE AT BS 720, LBL 5 TO RBL 5 BETWEEN 28L AND 28R, WL 138 TO BE CORRODED AND OUT OF LIMITS.Apr 27, 1998 · N265FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00298Floorbeam · corrodedCORROSION (C53-224-01) ON FLOORBEAM AT BS 312, LBL 4, WL 208. *S/D* REPAIRED FLOORBEAM AT BS 312, LBL 4, WL 208 IAW FED-EX SRM 53-10-8, 53-10-1, BAC DRAWING 65-16314.Apr 27, 1998 · N265FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 98FDEA00297Floorbeam · corrodedCORROSION (C53-111-01) ON FLOORBEAM LOWER CHORD AT BS 1070, LBL 42, RBL 50, WL 200. *S/D* REPAIRED LOWER CHORD ON FLOORBEAM BS 1070, LBL 42 TO RBL 50, WL 200 IAW FED-EX SRM 53-10-8, 53-10-1.Apr 27, 1998 · N265FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 98FDEA00305Strap · gougedNR 0960 BEAR STRAP AT LOWER HINGE CUTOUT FOR FWD ENTRY DOOR IS DEEPLY GOUGED. GOUGE DAMAGE WAS BLENDED OUT PER SRM 51-10-1, AREA WAS EDDY CURRENT INSP, NO CRACKS WERE FOUND. SKIN WAS THEN REPAIRED PER EA 7-5330-29483, DATED 4-22-98. BASED ON S/B 727-53-198,Apr 25, 1998 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00304Bellframe · crackedNR NR 0211 - 72-C236-02, BS 804, STR 14L, BELLFRAME ANGLE IS CRACKED AT FASTENER UPPER LOBE. REMOVED DAMAGED AREA OF BELLFRAME DYE CHECKED FOR VERIFICATION. INSTALLED REPAIR FILLER AND DOUBLER PER SRM 51-40-3 PG 3.Apr 25, 1998 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00294Shear Tie · corrodedWHILE WORKING NR 0450 FOUND SHEAR TIE BS 700 STRINGER 28R TO 28L CORRODED. *S/D* REPLACED SHEAR TIE BS 700, STR 28R TO 28L IN ACCORDANCE WITH FED-EX SRM 51-20-1, 51-30-2, BAC DRAWING 65-15938.Apr 25, 1998 · N265FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00293Floorbeam · corrodedNR 0454 014, CORROSION (C53-224-01(2)) ON LONGITUDINAL BEAM AT RBL 45, BS 760-800, WL 208, I/B FLANGE. REMOVED CORROSION ON LONGITUDINAL BEAM RBL 45, BS 760-800. FOUND TO BE OUT LIMITS, PER FEDEX SRM 53-10-1. REMOVED AND REPLACED LONGITUDINAL FLOORBEAM PERApr 24, 1998 · N265FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 98FDEA00292Skin · crackedNR 0141 013, LEFT HAND SERVICE DOOR OUTER SKIN IS CRACKED APPROX .75 AT LWR FWD CORNER, CRACK IS GOING THROUGH FASTENER. REPAIRED L/SERVICE DOOR OUTER SKIN, LWR FWD CORNER IAW FEDEX SRM 52-40-2 PG 1, 5.Apr 24, 1998 · N265FE · Boeing 727233 · Service DoorsSDR 98FDEA00291Frame · crackedNR 0240 012, NR 3 LWR CARGO DOOR FWD FRAME IS CRACKED IN O/B RADIUS, AT LWR STOP FITTING. REMOVED AND REPLACED LWR FWD NR 3 CARGO DOOR FRAME IAW FEDEX SRM 51-30-2 AND 51-10-1.Apr 24, 1998 · N265FE · Boeing 727233 · Cargo/Baggage DoorsSDR 98FDEA00290Frame · gougeGOUGE IN FRAME AT BS 1090, LBL 60, WL 182. *S/D* REPAIRED FRAME AT BS 1090, LBL 60, WL 182 PER FED-EX SRM 51-40-3.Apr 24, 1998 · N265FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00289Floorbeam · corrodedCORROSION (C53-224-03-1/2) ON FLOORBEAM AROUND NUT PLATE HOLE BS 344, RBL 12, WL 208. *S/D* REPAIRED FLOORBEAM UPPER CHORD AT BS 344, RBL 68 TO LBL 68 PER FED-EX SRM 51-30-2, FEDEX DRAWING SR 27-53-007.Apr 24, 1998 · N265FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 98FDEA00306Keel Beam · crackedNR 0638, NR 71-C304-02, KEEL BEAM AREA LWR RT KEEL BEAM CRACKED, JUST ABOVE LWR RT FITTING APPROX BS 875. TRIMMED THE UPPER FLANGE OF KEEL BEAM CHORD, REMOVING CRACKED AREA. TREATED AND PRIMED METAL. INSTALLED REPAIR DOUBLER PER BOEING SERVICE BULLETIN 727-Apr 23, 1998 · N267FE · Boeing 727233 · Fuselage Main, KeelSDR 98FDEA00307Frame · gougedNR 0227, BS 380, BELOW STR 5L, FRAME GOUGED ON INBD SIDE OF INBD LEG OF FRAME. REMOVED DAMAGE AND INSTALLED DOUBLER PER SRM 53-10-4.Apr 22, 1998 · N227FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00286Clip · corrodedLWR FRAME TO WEB CLIP CORRODED AT BS 681 LBL 3 WL 156. *S/D* CORRODED LOWER FRAME TO WEB CLIP AT BS 681, LBL 3, WL 156. FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REPLACED CORRODED LOWER FRAME TO WEB CLIP AND REINSTALLED PARTS REMOVED FOR ACCESS IAApr 20, 1998 · N265FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00285Floorbeam · corrodedCORROSION (C53-224-01, 2) ON UPPER CHORD OF BS 950 FLOORBEAM LBL 16 TO 19 WL 208. *S/D* REPAIRED CORROSION AREAS OF UPPER CHORD BS 950 FLOORBEAM FROM LBL 16 TO 19, WL 208 PER EA NR 7-5310-38742.Apr 20, 1998 · N265FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 98FDEA00284Stringer · corrosionCORROSION ON STR 28R BS 710 WL 140. *S/D* REMOVED CORRODED STRINGER 28 RT, BS 710 TO 720 AND INSTALLED NEW SECTION AND REPAIR CAP AT BS 710 IAW FED-EX SRM 53-10-3.Apr 20, 1998 · N265FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 98FDEA00283Beam · corrosionCORROSION (C53-224-01, 2) ON LONGITUDINAL BEAM FLANGES AT RBL 24 BS 760 TO 790 WL 208. *S/D* REMOVED AND REPLACED LONGITUDINAL BEAM UPPER CHORD BS 740 TO 850, RBL 25 AND SEAT TRACK BS 760 TO 850, RBL 25, WL 208 PER FED-EX SRM 51-30-2 AND FED-EX DRAWING 65-16Apr 20, 1998 · N265FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00282Skin · corrodedCORROSION ON SKIN FWD CARGO BAY BS 700 TO 720 RBL 10 WL 138 NEXT TO STR 28R. *S/D* REMOVED CORRODED SKIN AT BS 700 TO 720, WL 138, RBL 10 AND INSTALLED INTERNAL DOUBLER. INSTALLED ALL ITEMS REMOVED FOR ACCESS IAW FED-EX SRM 53-30-3.Apr 20, 1998 · N265FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 98FDEA00281Skin · corrodedWHILE WORKING ON NR0518, FOUND CORROSION ON SKIN AT BS 683 LBL 12 WL 138, BET 27L TO 28L. *S/D* REPAIRED SKIN AT BS 683, LBL 12, WL 138, BETWEEN STR 27L AND 28L PER FED-EX SRM 53-30-3.Apr 20, 1998 · N265FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 98FDEA00280Shear Tie · corrodedNR0573: WHILE WORKING NR0450 FOUND SHEAR TIE AT BS 720, LBL 5 - RBL 5 BETWEEN 28L-R WL 138 TO BE CORRODED AND OUT OF LIMITS. REMOVED CORRODED SHEAR TIE AND FABRICATED NEW AND INSTALLED IAW BAC DRW 65-15939 AND FEDEX SRM 51-20-1 AND 51-20-2.Apr 20, 1998 · N265FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00279Support · corrodedNR 0577: WHILE WORKING NR-0573 FOUND 25 G-BEAM TO BE CORRODED AT BS 266 LBL 8 WL 208. REMOVED AND REPLACED 25 G-BEAM BS 266 LBL 8 - RBL 21.5 W 208 IAW FEDEX SRM 53-10-1, 51-30-2, FEDEX MM 57-20-21.Apr 20, 1998 · N265FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00277Skin · corrodedNR-0402, LWR FUSELAGE SKIN CORRODED ON UPPER SURFACE AT BS 663 BL0, WL 138.Apr 17, 1998 · N265FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 98FDEA00258Splice · corrodedNR 0789 70C079-00, BS 720D - 720E, STR 21R IN SNAKE PIT AREA CORRODED. CUTOUT CORRODED AREA AND INSTALLED STR SPLICE PER SRM 53-10-3, PAGE 3.Apr 7, 1998 · N222FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00248Beam · corrodedA/C BAY CORROSION ABOVE DELTA BEAM BS 750, RBL 6, AROUND ACCESS PLATE 3210. REMOVED CORROSION, TREATED, INSTALLED DOUBLER OVER AREA PER SRM 51-40-2.Apr 2, 1998 · N222FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00247Beam · corrodedA/C BAY, BS 743, RBL 8 HEAVY CORROSION ABOVE DELTA BEAM, LWR SURFACE OF PLATE AT FWD ROW OF FASTENERS. REMOVED CORROSION, TREATED, INSTALLED DOUBLER PER SRM 51-40-02 OVER DAMAGED AREA.Apr 2, 1998 · N222FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00245Frame · dentedUPPER LOBE BS 580, RBL 65 BELL FRAME DENTED. REMOVED DAMAGED AREA OF BELL FRAME. INSTALLED DOUBLER PER EA 7531028295 AND SRM 53-40-3.Apr 2, 1998 · N222FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00244Frame · dentedUPPER LOBE, BS 600, RBL 65 BELL FRAME DENTED. REMOVED DAMAGED AREA OF BELL FRAME. INSTALLED DOUBLER PER EA 7531028295 AND SRM 53-40-3.Apr 2, 1998 · N222FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00243Frame · dentedUPPER LOBE BS 540, RBL 65, BELL FRAME DENTED. REMOVED DAMAGED AREA OF BELL FRAME. INSTALLED DOUBLER PER EA 7531028295 AND SRM 53-40-30.Apr 2, 1998 · N222FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00242Skin · corrodedFUSE SKIN CORRODED AT BS 660 BETWEEN STR 28L TO W8R. REMOVED CORROSION. REMOVED SECTION OF FUSE SKIN I/B OF STR 28R. INSTALLED REPAIR DOUBLER PER SRM 53-30-3.Apr 2, 1998 · N222FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 98FDEA00246Beam · corrodedA/C BAY, BS 743 CHORD ABOVE DELTA BEAM, UPPER SURFACE CORRODED LBL - RBL 12. REMOVED CHORD ANGLE AND REINSTALLED WITH NEW CHORD ANGLE PER SRM 51-30-2.Apr 1, 1998 · N222FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 98FDEA00241Frame · dentedUPPER LOBE BELTFRAME AT BS 500, RBL 65 DENTED OUT OF LIMITS PER EA 7531028295. REMOVED DAMAGE AT BELTFRAME BS 500, RBL 65 AND INSTALLED DOUBLER PER SRM 51-40-3 PG 1-6 AND EA 7531028295.Mar 27, 1998 · N222FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00240Frame · dentedUPPER LOBE, BELTFRAME AT BS 520, RBL 65 DENTED OUT OF LIMITS. REMOVED DAMAGE AT BELTFRAME BS 520, RBL 65 AND INSTALLED DOUBLER AS PER SRM 51-40-3 PG 1-6 AND EA 7531028295.Mar 27, 1998 · N222FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00212Frame · wornNR 0978 71C 701 - LWR AFT CARGO, FUSE BS 1148, UPPER BELTFRAME FLANGE WORN IN EXCESS OF 50 PERCENT NEAR STR 22 LEFT. BLENDED OUT DAMAGE AND INSTALLED DOUBLER PER SRM 51-40-3.Mar 20, 1998 · N268FE · Boeing 727233 · Fuselage Main, FrameSDR 98FDEA00216Stringer · corrodedNR 0228 71C 709-02, LOWER LOBE AFT CARGO CORROSION ON OUTBD FLANGE OF STR 29L FROM BS 950E TO BS 990. INSTALLED STRINGER REPAIR ON STRINGER 29L 950E TO 990 PER EA 7-5310-29401 DATED MARCH 07, 1998.Mar 19, 1998 · N263FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR 98FDEA00215Skin · damagedRT OUTBD AILERON HAS .25 INCH DIAMETER CHERRY MAX IN UPPER SKIN, COUNTER SINK IS TOO DEEP, IN SKIN .040 THICK. REMOVED DAMAGE AND INSTALLED FLUSH DOUBLER PER SRM 57-50-5 AND CUT OUT RIB AREA TO FACILITATE DOUBLER AND INSTALLED TYPICAL FORMED SECTION REPAIR TOMar 18, 1998 · N268FE · Boeing 727233 · AileronsSDR 98FDEA00214Rivets · looseNR 0324, RT WING OUTBOARD AILERON HAS APPROX 70 RIVETS WORKING AND LOOSE ALONG UPPER SKIN FRONT SPAR ATTACHMENT. REMOVED AND REPLACED RIVETS PER EA 7-5750-29411, SRM 57-50-5 SRM 51-30-2.Mar 18, 1998 · N268FE · Boeing 727233 · AileronsSDR 98FDEA00211Skin · damagedNR 0905, RT OUTBD AILERON HAS .25 INCH DIAMETER CHERRY MAX FASTENER IN UPPER SKIN, RIB IS .600 WIDE, ORIGINAL FASTENERS WERE .125 INCH DIAMETER, COUNTER SINK INTO RIB WILL HAVE DAMAGED RIB AND MINIMUM ED IS LOST IN RIB. REMOVED AND REPLACED RIB PER SRM 51-10-Mar 18, 1998 · N268FE · Boeing 727233 · Ailerons
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