Boeing 727-2S2F

Service difficulty reports · 842

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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 = '7272S2F'
  ORDER BY difficulty_date DESC"

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SDR 07FDEA05060Actuator · failedAFTER T/O, NON FLYING PILOT SELECTED FLAPS FROM 5 DEG TO 2 DEG CREW NOTICED AN ILLUMINATED LE FLAPS AMBER LIGHT WITH ASSOCIATED LOSS OF SYS A HYDRAULIC FLUID. SO FLAP CONFIGURATION PANEL INDICATED AN AMBER NR 4 SLAT. CREW FOLLOWED ALL APPLICABLE QRH PROCEDURDec 15, 2007 · N207FE · Boeing 7272S2F · Trailing Edge Flap ActuatorSDR 07FDEA05001Windshield · crackedAT APPROX 27000' ON CLIMB-OUT, CAPT'S L-1 WINDOW CRACKED/SHATTERED AND BEGAN ARCING. COMPLIED WITH RED TABS PROCEDURES. RETURNED TO MEMPHIS. REMOVED CAPT'S NR 1 WINDOW AND COMPLIED WITH PREPARATION FOR INSTALL IAW B727-200 AMM 56-11-011-4. COMPLETED INSTALDec 3, 2007 · N213FE · Boeing 7272S2F · Flight Compartment WindowsSDR 07FDEA04548Transmitter · looseNR 2 LOW OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED IN DESCENT FOLLOWED BY OIL PRESSURE DROP TO ZERO. QRH PERFORMED, ENGINE SHUT DOWN WITH OIL PRESSURE AT 5 TO 10 PSI OIL QUANTITY NORMAL. TEMP RISING GRADUALLY ENGINE SHUTDOWN 13 MINUTES AFTER FIRST INDICATOct 10, 2007 · N204FE · Boeing 7272S2F · Engine Oil QuantitySDR 07FDEA04481Channel · crackedTHE RT WING TIP FWD FAIRING NUT PLATE CHANNEL IS CRACKED. THIS DISCREPANCY WAS DISCOVERED WHILE COMPLYING WITH NON-ROUTINE NR N00015. REPLACED CHANNEL IAW NR 7-5730-115028. REMOVED AND REPLACED NUTPLATE CHANNEL.Oct 3, 2007 · N205FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 07FDEA04480Channel · crackedTHE RT AFT WING TIP SECTION HAS A BROKEN NUT PLATE CHANNEL IN THE LOWER AFT END. THIS DISCREPANCY WAS FOUND DURING A "B" CHECK. REPAIRED NUTPLATE CHANNEL PER EA NR 7-5730-115028Oct 3, 2007 · N205FE · Boeing 7272S2F · Wing Miscellaneous StructureSDR 07FDEA03799Circuit Breaker · failedIN CRUISE SMELL OF SMOKE AND THE SIGHT OF SMOKE COMING FROM BACK OF S/O PANEL. SMOKE MOVED TOWARD F/O SEAT. THE SMELL WAS LIKE CAR EXHAUST. RAN ALL FUMES AND ODORS CHECK LIST. ALSO SHUT OFF GASPER FAN. THE SMOKE ONLY LASTED FOR AROUND 15 SEC. NO OTHER ISep 15, 2007 · N217FE · Boeing 7272S2F · Fire Protection System WiringSDR 07FDEA03308Indicator · shortedDURING CLIMB-OUT OF FL220, NR 2 FUEL ICING LIGHT CAME ON. RAN QRH PROCEDURE, FUEL TEMP WAS 40 DEGREES, RETURNED TO MEMPHIS, DUMPED FUEL AND FUEL ICING LIGHT REMAINED ON THROUGH LANDING, WENT OUT WHILE WAITING TO PARK. FOUND BULB ASSY BENT CAUSING BULB TO SHOSep 2, 2007 · N210FE · Boeing 7272S2F · Engine Fuel Indicating SystemSDR 07FDEA02885Channel · crackedLT WING AR T/E REAR SPAR AREA APPROX RS STA491. LOWER FIXED PANEL UPPER INBD CHORD MOUNT BRACKET HAS A CRACK BELOW SPOILER PNL NR 3. REMOVED AND REPLACED BRACKET IAW SRM 51-30-2.Aug 14, 2007 · N212FE · Boeing 7272S2F · Wing Miscellaneous StructureSDR 07FDEA02816Skin · crackedRT WING NR 8 SLAT UNDERSIDE SKIN AT OTBD END HAS SEVERAL SHEARED FASTENERS AND A POSSIBLE CRACK AT ONE OF THE FASTENER HOLES. REMOVED AND REPLACED NR 8 SLAT ASSY IAW 27-81-011-4.Aug 9, 2007 · N212FE · Boeing 7272S2F · Leading Edge DevicesSDR 07FDEA02804Skin · misrepairedREPAIR ON RT WING OB AFT FLAP LWR SIDE AT W-STA 650. REPAIR EVALUATED AND FOUND NOT TO BE IAW SRM 51-40-20. PREVIOUSLY INSTALLED REPAIR WAS REMOVED AND REPAIRED IAW SRM 51-40-20.Aug 8, 2007 · N212FE · Boeing 7272S2F · Trailing Edge FlapsSDR 07FDEA02803Panel · crackedRT WING REAR SPAR LWR CHORD WAVY PANEL HAS 2 EA CRACKS APPROX FROM RSS 542-RSS 563. REMOVED SEAL IAW SRM 51-30-2. FABRICATED NEW SPLICES ON TRAVELER T7/691015 2024 T3 .063. FABRICATED LWR CHORD PANEL OB SIDE ON TRAVELER T7/691016 2024 T3 .063. INSTALLED REAug 8, 2007 · N212FE · Boeing 7272S2F · Wing, Plate/SkinSDR 07FDEA02802Support Angle · crackedRT WING OB T/E LOWER PANEL SUPPORT ANGLE HAS A CRACK UNDER SPOILER NR 13. REMOVED AND REPLACED SUPPORT ANGLES IAW SRM 51-30-2.Aug 8, 2007 · N212FE · Boeing 7272S2F · Wing Main, Frame StructureSDR 07FDEA02785Angle · corrodedLOWER FUSELAGE ANGLE BRACKET SUPPORT HAS HEAVY CORROSION AT STA 804 - STA 825.94 LBL 0 CUT OUT DAMAGED AREA IAW SRM 51-40-3. FABRICATED 9 REPAIR PARTS IAW SRM 51-40-4. LOCATED AND DRILLED IAW SRM 51-30-5, TREATED AND PRIMED IAW SRM 51-10-2, AND INSTALLED AAug 7, 2007 · N212FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 07FDEA02638Skin · delaminatedLT WING IB AFT FLAP DISBONDED AT IB END REMOVED AND REPLACED FLAP ASSY IAW MM 27-51-002-4.Jul 27, 2007 · N212FE · Boeing 7272S2F · Trailing Edge FlapsSDR 07FDEA02510Switch · failedUPON FLAP RETRACTION TO 2 THE NR 5 SLAT REMAINED EXTENDED WITH AMBER LIGHT ON FORWARD LED INDICATOR PANEL. S/O LED INDICATOR PANEL SHOWED NR 5 SLAT EXTENDED. QRH WAS FOLLOWED WITH ALL PROCEDURES COMPLIED WITH. RETURNED TO MEM FOR UNEVENTFUL LANDING. REMOVEJul 18, 2007 · N210FE · Boeing 7272S2F · Leading Edge Slat Control SystemSDR 07FDEA02397Rod End · shearedLANDING AT GTF, THE NOSE GEAR WOULD NOT EXTEND. RAN THE QRH EXTENDED THE GEAR MANUALLY. FOUND LOCK ACTUATOR RODEND SHEARED OFF. REPLACED NOSE GEAR LOCK ACTUATOR PER MM 32-33-011-4. OPS CHECKS NORMAL. PREMATURE REMOVAL/INSTALLATION OFF MFG 65-40467-6, SRL Jul 8, 2007 · N215FE · Boeing 7272S2F · Landing Gear ActuatorSDR 07FDEA02298Landing Gear · unknownWHEN CONFIGURING FOR LANDING, NOSE GEAR STAYED UP. GO AROUND INITIATED AND NOSE GEAR EXTENDED BEFORE QRH STARTED. HYD PRESSURE NORMAL THROUGH-OUT. WHEN NOSE GEAR DID EXTEND, DOOR LIGHT CAME ON FOR ABOUT 20 SECS BEFORE GEAR CAME DOWN. INSP NLG, WHEEL WELLJun 27, 2007 · N201FE · Boeing 7272S2F · Nose/Tail Landing GearSDR 07FDEA02107Frame · damagedFS 348.2 6 INCHES ABOVE UPPER AFT DOOR STOP HAS A DRILL START ON FUSELAGE FRAME FOUND DURING REMOVAL OF COVER TO WORK DOOR STOP FITTING. INSTALLED FABRICATED REPAIR ANGLE REF SRM 51-40-3 VERIFIED MATERIAL 2024 .080 (O), HEAT TREATED ANGLE, FABRICATED VERIFIEDJun 11, 2007 · N210FE · Boeing 7272S2F · Fuselage Main, FrameSDR 07FDEA02101Frame · misrepairedFOUND ON AGING A/C INSP FOUND EXISTING REPAIR AT STA 760 FRAME DOES NOT CONFORM TO SB 727-53-0197. REMOVED AND DISCARDED EXISTING REPAIR. ACCOMPLISHED HFEC OF DAMAGE. FABRICATED REPAIR PARTS AND INSTALLED, REF FED EX EA 7-5310-113044.Jun 9, 2007 · N210FE · Boeing 7272S2F · Fuselage Main, FrameSDR 07FDEA02097Frame · misrepairedAGING A/C INSP, FOUND FRAME REPAIR AT STA 520, STR 16R-17R, DID NOT CONFORM TO SRM 51-40-3 FIG 1. REMOVED AND DISCARDED PREVIOUS REPAIR ANGLES AND INSTALLED NEW REPAIR PARTS REF. ALL WORK ACCOMPLISHED ON WO#36350/N00878.Jun 9, 2007 · N210FE · Boeing 7272S2F · Fuselage Main, FrameSDR 07FDEA02076Tab · delaminatedRIGHT WING INBD AILERON TAB OTBD AFT AREA HAS 1" AREA OF DELAM REMOVED AND REINSTALLED R/W INBD AILERON TAB REF MM 27-10-011-4 ADJ/CHECK REF MM 27-10-000-5, OPS CHECK GOOD.Jun 6, 2007 · N210FE · Boeing 7272S2F · Aileron TabsSDR 07FDEA02043Floorbeam · corrodedCABIN FLOORBEAM HAS CORROSION STA 344 LBL 36" TO 54" REMOVED CORROSION, ORIGINAL MATERIAL .107, REMAINING .086", ROTO PEENED AREA. TREATED AND PRIMED AREA REF 51-10-02, MM 51-20-151 AND SOPM 20-10-03, AND EA NR 7-5310-111639.Jun 2, 2007 · N210FE · Boeing 7272S2F · Fuselage Main, Floor BeamSDR 07FDEA02027Skin · crackedRIGHT WING UPPER TE SKIN CRACKED AT NR 12 SPOILER IB CENTER HINGE CUTOUT REMOVED NR 12 SPOILER. REMOVED FASTENERS IN REPAIR AREA. STOP DRILLED CRACK, NDT VERIFY CRACK TERMINATION. FABRICATED REPAIR PLATE, TREATED AND PRIMED. INSTALLED REPAIR, APPLIED FILLEMay 31, 2007 · N210FE · Boeing 7272S2F · SpoilersSDR 07FDEA02026Structure · misrepairedON AGING A/C INSPECTION, FOUND EXISTING REPAIR LOCATED AT STA 520, STR 16R-17-R, DID NOT CONFORM TO SRM. REMOVED AND DISCARDED PREVIOUS ANGLES & INSTALLED NEW REPAIR PARTS, EA I070369 ALL WORK ACCOMPLISHED ON WO 36352/N00878.May 31, 2007 · N210FE · Boeing 7272S2F · Fuselage Main, StructureSDR 07FDEA02023Frame · corrodedAFT PIT, AFT BULKHEAD SUPPORT FRAME IS CORRODED AT FASTENER RECEPTACLE BS 1166, LBL 19-RBL 36, WL 179 REMOVED CORROSION, FOUND 3 AREAS TO BE OUT OF LIMITS, IAW SRM 53-10-1. REMOVED DAMAGED AREA, FABRICATED REPAIR PART OUT OF 7075-T6 .063. FABRICATED FILLERS May 30, 2007 · N210FE · Boeing 7272S2F · Fuselage Main, FrameSDR 07FDEA02022Intercostal · crackedLT AFT WING BODY FILLET B HYD SYS SVC BAY FRG FRAME INTERCOSTAL IS CRACKED AT NR 1 EMDP PRESSURE HOSE BHD FITTING CUTOUT OB HYD RESERVOIR BS 950A 5, STR 23L. REMOVED DAMAGED INTERCOSTAL REF SRM 51-30-2 MFG NEW INTERCOSTAL REF DWG 69-14299, AND INSTALLED NEW May 30, 2007 · N210FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 07FDEA02024Tab · delaminatedRIGHT WING OTBD AILERON TAB HAS A 37" LONG AREA OF DELAM FROM OTBD EDGE. REMOVED AND REPLACED R/W OTBD AILERON TAB REF M/M 27-10-041-4. PERFORMED ADJ/TEST REF MM 27-10-000-5, OPS CHECK GOOD.May 30, 2007 · N210FE · Boeing 7272S2F · Aileron TabsSDR 07FDEA02016Skin · crackedLOWER FUSELAGE VHF NR 2 ANTENNA, SKIN ON FWD LIP DAMAGED, AND BASE PNL FOR ANTENNA IS CRACKED SRM 51-30-2. REMOVED VHF ANTENNA PANEL, REPLACED HAT CHANNEL AND INSTALLED PANEL SRM 51-30-2.May 30, 2007 · N210FE · Boeing 7272S2F · Fuselage Main, Plate/SkinSDR 07FDEA01989Attach Fitting · crackedMAIN DECK BODY FRAME INTERCOSTAL ASSY CLIP IS CRACKED BS 348 AFT, STR 15L. REMOVED PANEL FWD OF STR 15L, STA 348, REMOVED DOOR STOP, REF SRM 51-30-2 FIG 1. REMOVED DAMAGE CLIP, NEW CLIP INSTALLED ON N/R N00991 WIP NR 4, DOOR STOP. REINSTALLED ON N/R N00991 May 26, 2007 · N210FE · Boeing 7272S2F · Fuselage Main, Attach FittingsSDR 07FDEA01933Skin · crackedRT WING, UPPER WING SKIN CRACKS AT NR 12 I/B HINGE CUT OUT. STOP DRILLED CRACK, NDT VERIFIED CRACK TERMINATION, FABRICATED AND INSTALLED REPAIR DOUBLER REF SRM 57-30-4.May 22, 2007 · N210FE · Boeing 7272S2F · Wing, Plate/SkinSDR 07FDEA01932Channel · corrodedAT LWR CARGO BAY, BS 1137-1140, RBL 61-62, WL 208, FLOOR SUPPORT CHANNEL I/B FLANGE LOWER SURFACE IS CORRODED. REMOVED SEAT TRACK REF SRM 51-30-02. REMOVED SIDEWALL PANEL, REMOVED SEAT TRACK SUPPORT CHANNEL. FABRICATED NEW PARTS, TREATED, PRIMED AND PAINTEDMay 22, 2007 · N210FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 07FDEA01931Support Angle · corrodedAFT PIT, STA 1166, WL 200, RBL 48, AFT WALL SUPPORT ANGLE, IS CORRODED UPPER AFT CORNER. BLENDED CORROSION AND FOUND ANGLE TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW ANGLE, REF SRM 51-30-2 PG 1-4, AND BOEING DWG NR 65-67251.May 22, 2007 · N210FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 07FDEA01930Deflector · crackedPNL RACK RT WING TO BODY RT WING TO BODY PLN UPPER SURFACE HAS A CRACKED BRACKET. PAINTED AND INSTALLED NEW PARTS, REF SRM 51-30-023 PG 1.May 22, 2007 · N210FE · Boeing 7272S2F · Wing Miscellaneous StructureSDR 07FDEA01929Support Angle · crackedLT WING T/E ANGLE SUPPORT FOR JACKSCREW MOST OUTBD FAIRING IS CRACKED FROM FASTENER HOLE (INBD ANGLE). REPLACED WITH NEW DOUBLER REF 51-30-5 AND SRM 51-30-2.May 22, 2007 · N210FE · Boeing 7272S2F · Wing Miscellaneous StructureSDR 07FDEA01855Frame · dentedAFT PIT STA 1130, LBL 25, STR. 26, FRAME IS DENTED CUT OUT DAMAGE, FABRICATED REPAIR ANGLE FROM 7075-0 .063 AND HEAT TREATED TO 7075-T-6 INSTALLED REPAIR ANGLE REF SRM 51-40-03.May 19, 2007 · N210FE · Boeing 7272S2F · Fuselage Main, FrameSDR 07FDEA01854Panel · damagedRT LOWER I/B PNL NR 9214 IS DAMAGED ON HORIZ STAB. REPAIRED RT HORIZONTAL STAB PANEL NR 9214 REF SRM 55-20-3 FIG 1 AND SRM 55-10-2 PG 1, FIG 1, SHT 1.May 19, 2007 · N210FE · Boeing 7272S2F · Horizontal Stabilizer, Plate/SkinSDR 07FDEA01853Flap Track · wornLT WING TE IB FLAP OB TRACK UPP OB FLG WEAR STEP HAS GOUGES/ HIGH METAL 5" - 32" FROM AFT END. LT WING INBD T/E FLAP OUTBD (NR 3) FLAP TRACK REPLACED ON W/C 27X5705-03.May 19, 2007 · N210FE · Boeing 7272S2F · Trailing Edge FlapsSDR 07FDEA01852Support Angle · crackedRT WING OB TE LWR SURFACE PANEL SUPPORT ANGLE CRACKED, 4" FWD OF TE, BELOW OB HINGE OF NR 12 SPOILER REPLACED PANEL SUPPORT ANGLE REF SRM 51-30-02 PAGE 19.May 19, 2007 · N210FE · Boeing 7272S2F · Wing Miscellaneous StructureSDR 07FDEA01851Flap Track · corrodedRT WING TOP SIDE OF I/B FLAP O/B FLAP TRACK AT MOUNT HOLE IS CORRODED RT I/B FLAP TRACK (NR 6) REPLACED. NEW TRACK INSTALLED ON W/C 27X5708-03.May 19, 2007 · N210FE · Boeing 7272S2F · Trailing Edge FlapsSDR 07FDEA01850Attach Angle · crackedLT WING, LWR TE PANEL BELOW NR 3 SPOILER PANEL, INBD SET OF ATTACH ANGLES FOR PANEL SUPPORT ROD OTBD ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE REFERENCING SRM 51-30-2.May 19, 2007 · N210FE · Boeing 7272S2F · SpoilersSDR 07FDEA01849Frame · dentedAFT CARGO PIT RT SIDE STA 1050 STR 25R FRAME IS DENTED DETERMINED DENT TO BE OUT OF LIMITS, PER SRM 53-10-01. FABRICATED REPAIR PARTS, TREATED AND PRIMED AND INSTALLED REF SRM 51-40-3 FIG 1, SRM 51-30-02.May 19, 2007 · N210FE · Boeing 7272S2F · Fuselage Main, FrameSDR 07FDEA01848Spar · crackedRT STAB AFT SPAR 3RD BALANCE BAY FROM O/B END, HINGE PANEL FWD ATTACH BRACKET CRACKED AT I/B END REPLACED CHANNEL AND WEB REF SRM 51-30-3 PG 5.May 19, 2007 · N210FE · Boeing 7272S2F · Horizontal Stabilizer, Spar/RibSDR 07FDEA01844Bracket · crackedLT WING TRAILING EDGE SMALL U SHAPE BRACKET FOR SUPPORT OF OUTBD TRACK FAIRING, IS CRACKED AT THE SERRATIONS INBD FLANGE REMOVED CLIP REF SRM 51-30-02 FIG.7 PG.32 INSTALLED NEW CLIP REF. SRM 51-30-02 PG 2May 18, 2007 · N210FE · Boeing 7272S2F · Wing, Attach FittingsSDR 07FDEA01845Seal Depressor · gougedFUSE LWR LOBE AFT CARGO DR FRAME INTERIOR SURFACE IS GOUGED AT LOWER AFT CORNER, BS 989, STR 26R. REMOVED AND INSTALLED NEW LOWER AFT CORNER, OF AFT CARGO PIT DOOR REF SRM 51-30-2 PG 1-12 (SEAL DEPRESSOR).May 18, 2007 · N210FE · Boeing 7272S2F · Fuselage Main, StructureSDR 07FDEA01843Tee Fitting · crackedMAIN UPPER CARGO DOOR S/N 9, TEE SUPPORT FITTING CRACKED AT LATCH HOOK 3RD FWD FROM AFT EDGE BY TORQUE TUBE BEARING FITTING. REMOVED AND REPLACED DAMAGED T- FITTING WITH NEW TEE CLIP FX797 IAE SRM 51-30-2.May 18, 2007 · N210FE · Boeing 7272S2F · Cargo/Baggage DoorsSDR 07FDEA01837Flap Track · corrodedLT WING TE IB FLAP OB TRACK IS CORRODED AT FWD END AND SPOILER SPPT ATTACH POINT LT WING INBD T/E FLAP OUTBD (NR3) FLAP TRACK REPLACED ON FED EX W/C 27X5705-03.May 17, 2007 · N210FE · Boeing 7272S2F · Trailing Edge FlapsSDR 07FDEA01836Frame · corrodedFUSELAGE LOWER LOBE NH NOSE TUNNEL TORQUE BOX INTERIOR HORIZ WEB IB CHORD IS CORRODED/EXFOILATION, BS 295-301, LBL 15, WL168 BLENDED AND REMOVED CORROSION .018 MATERIAL LOSS, WITHIN LIMITS, APPLIED ALODINE AND PRIMER REF SRM 51-10-1 AND SRM 51-10-2, SRM 53-10May 17, 2007 · N210FE · Boeing 7272S2F · Fuselage Main, StructureSDR 07FDEA01828Frame · dentedFWD PIT FRAME, STA 720 DENTED BETWEEN STRINGER 23-24R REMOVED DAMAGE SECTION OF FRAME REF SRM 53-10-4 FIG 1. FABRICATED REPAIR PARTS REF SRM 53-10-4 FIG 1. DRILLED REPAIR PARTS REF 51-10-4, AND INSTALLED NEW REPAIR PARTS REF SRM 53-10-4 FIG 1.May 17, 2007 · N210FE · Boeing 7272S2F · Fuselage Main, FrameSDR 07FDEA01827Intercostal · crackedMAIN DECK BODY FRAME INTERCOSTAL ASSY CLIP IS CRACKED BS 351, STR 15L REMOVED AND REPLACED CLIP. REF SRM 51-30-2 PG 1-3 AND 5-7.May 17, 2007 · N210FE · Boeing 7272S2F · Fuselage Miscellaneous StructureSDR 07FDEA01822Stiffener · crackedANGLE CRACKED ON THE VERTICAL STAB LEADING EDGE WEB LOCATED ON THE UPPER RIGHT ON THE AFT SIDE OF WEB AND THE UPPER STAB BULKHEAD REMOVED AND REPLACED STIFFENER ANGLE ON VERTICAL STAB. REFERENCE SRM 51-30-02, PG 3.May 15, 2007 · N210FE · Boeing 7272S2F · Vertical Stabilizer
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