Boeing 757-236

Service difficulty reports · 2,544

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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 = '757236'
  ORDER BY difficulty_date DESC"

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SDR FDEA201406131424Floorbeam · corrodedBS 350 FLOORBEAM UPPER SURFACE CORRODED RBL 10 TO RBL 60. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. REPAIRED FLOORBEAM IAW SRM 53-00-51 FIG 201 REPAIR 3. MAJOR REPAIR.Jun 13, 2014 · N977FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA201406121412Crease Beam · corrodedRIGHT INBD CREASE BEAM UPPER SURFACE CORRODED BS 395. R & R CREASE BEAM ANGLE IAW SRM 51-40-02 & DWG 141N8422. MAJOR REPAIR.Jun 12, 2014 · N977FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201406101390Keelbeam · corrodedKEEL BEAM FITTING AT BS 1100 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-40-12 FIG 101 DET IV. LOCATED & DRILLED IAW SRM 51-40-05, AND INSTALLED.Jun 10, 2014 · N977FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201406071352Deck Plate · gougedMAIN CABIN AT BS 1680 RBL 9.20 DECK PLATE GOUGED. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-00-51, FIG. 101, DETAIL III. REMOVED AND REPLACED DECK PLATE, IAW SRM 51-40-02 AND DWG 146N5318. MAJOR REPAIR.Jun 7, 2014 · N977FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201406051320Seat Track · damagedSEAT TRACK BS 1180 - 1240 LBL 44 NICKED & GOUGEED ENTIRE LENGTH. REMOVED NICKS & GOUGES IAW SRM 53-00-52. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I. R & R SEAT TRACK IAW SRM 51-40-02 & DWG 146N5123.Jun 5, 2014 · N977FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201406031295Stiffener · damagedFLOORBEAM ATTACH STIFFENER HOLE ELONGATED AT BS 1660, BL 0. REMOVED STIFFENER IAW SRM 51-40-02. FOUND TO BE OUT OF LIMITS IAW SRM 51-40-06 FIG 3 TABLE I. INSTALLED STIFFENER IAW SRM 51-40-02.Jun 3, 2014 · N977FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201405281213Governor · malfunctionedLEFT ENGINE WOULD NOT SET TAKEOFF POWER, WOULD ROLL BACK. LT ENGINE FUEL FLOW GOVERNOR & HP FUEL PUMP R & R. ENG RUN AT HIGH POWER IAW JRH WITH THROTTLES MATCHED AT ALL POWER SETTINGS WITH NO SURGING.May 28, 2014 · N978FD · Boeing 757236 · Fuel Controlling SystemSDR FDEA201405211120Frame · dentedLEFT SIDEWALL FRAME HAS DENT AT STATION 1400, NEAR STRINGER 25L. EVALUATED FRAME STATION 1400, LT SIDE & DENTS NOT ALLOWED ON FLANGE IAW SRM 53-00-07, FIG 101, DETAIL II. R & R FRAME IAW SRM 51-40-02 & DWG 146N1011. FRAME WAS RECEIVED ON TRAVELER T14 1063426May 21, 2014 · N977FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA201405161048Floorbeam · corrodedFLOORBEAM TEE BS 1640 RBL 44 - 60 CORRODED ON THE BOTTOM SIDE OF THE TOP FLANGE. REMOVED CORROSION IAW SRM 51-10-02, & FOUND TO BE OUT OF LIMITS. R & R FLOORBEAM TEE AT BS 1640 IAW SRM 51-40-02, DWG 146N5089.May 16, 2014 · N977FD · Boeing 757236 · Fuselage Main, Floor BeamSDR FDEA201405100976Frame · gougedAFT CARGO BAY FRAME BS 1280, S29L - 29R GOUGED. REMOVED GOUGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00- 07, DETAIL II, FIG. 101. REMOVED AND REPLACED FRAME IAW SRM 51-40-02 AND DWG 146N1005. MAJOR REPAIR.May 10, 2014 · N977FD · Boeing 757236 · Fuselage Main, FrameSDR FDEA201405060954Battery Pack · dischargedEMERGENCY LIGHT ABOVE L1 DOOR DIM & GOES OUT. R & R BATTERY PACK FOR LT SIDE EMER LIGHT IAW AMM 33-51-07-2. OPERATIONS CHECKED NORMAL.May 6, 2014 · N979FD · Boeing 757236 · Emergency LightingSDR FDEA201405060952Switch · defectiveMETAL CLIP ON EMER LIGHTS SWITCH CAME LOOSE. SWITCH DOES NOT OPERATE NORMALLY AFTER SHUT DOWN. R & R EMER LIGHTS SWITCH IAW 33-51-08-4. OPERATIONS CHECKED GOOD, ACFT OK FOR SERVICE.May 6, 2014 · N978FD · Boeing 757236 · Emergency LightingSDR FDEA201405020914Engine · failedAT FL 390, ACFT SHUDDERED WITH A ASSOCIATED POP. EGT WENT INTO RED, FOR RT ENGINE. IMMEDIATELY BROUGHT RT THROTTLE TO IDLE. EGT WAS IN THE RED APPROX 15 SECONDS AFTER THROTTLE WAS AT IDLE, MOTOR RAN NORMALLY AT IDLE. CAPTAIN STATED THAT HE OBSERVED THE May 2, 2014 · N953FD · Boeing 757236 · Engine (Turbine/Turboprop)SDR FDEA201405010903Seat Track · gougedSEAT TRACK AT BS 440 LBL 45 HAS NICKS & GOUGES. FOUND SEAT TRACK AT LBL 45, STATION 440 - 680, TO BE OUT OF LIMITS, DUE TO DAMAGE EXCEEDING THE LIMITS GIVEN IN SRM 53-00-52 FIG 101 DETAIL I. SEAT TRACK REMOVED & INSTALLED ON STAM WC 118250302DSSR10. THIS NRMay 1, 2014 · N630SH · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201404300895Seat Track · corrodedMAIN DECK BS 780 - 880 LBL 45.50 SEAT TRACK HAS CORROSION, NICKS & SCRATCHES. REMOVED DAMAGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG. 101, DETAIL I. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 AND DWG 143N5080. MAJOR.Apr 30, 2014 · N977FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201404300898Crease Beam · corrodedMAIN DECK COMPARTMENT STATION 780 - 800, RT SIDE CREASE BEAM, INNER CHORD DAMAGED. REMOVED CORROSION & DAMAGE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL VIII. R & R RT INBD CREASE BEAM CHORD IAW SRM 51-40-02 & DWG 143N5520,Apr 30, 2014 · N977FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA201404240838Skin · dentedLOWER FUSELAGE SKIN HAS A DENT AT BS 1478 BETWEEN STRINGERS 27 & 28L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-00-01 REPAIR 16.Apr 24, 2014 · N960FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201404210781Crease Beam · corrodedMAIN CABIN AT BS 1260 RT INBD CREASE BEAM CORRODED. BLENDED CORROSION IAW SRM 53-40-13. FOUND TO BE OUT OF LIMITS IAW SRM 53-40-13 FIG 101 DETAIL II. REPLACED CREASE BEAM IAW SRM 51-40-02 & DWG 146N5590. REPAIR CLASSIFIED AS CATEGORY A MAJOR.Apr 21, 2014 · N630SH · Boeing 757236 · Fuselage Main, StructureSDR FDEA201403280595Actuator · failedDURING DEPARTURE, WHEN FLAPS SELECTED TO UP THE LE SLAT DISAGREE EICAS CAME ON. THE LE DISCREET LIGHT ILLUMINATED. R & R NR 6 OTBD LE SLAT DRIVE ROTARY ACTUATOR IAW MM 27-81-18-4. OPS CHECKED GOOD.Mar 28, 2014 · N940FD · Boeing 757236 · Leading Edge Slat ActuatorSDR FDEA201403050446Windshield · crackedFL 350, RT FWD WINDOW CRACKED WITH VISIBLE ARCING IN LOWER LEFT CORNER. REMOVED AND REPLACED WINDSHIELD IAW AMM 56-11-01-4.Mar 5, 2014 · N949FD · Boeing 757236 · Flight Compartment WindowsSDR FDEA201402280426Light · inoperativeAT DEPARTURE CREW COULD NOT GET R1 DOOR SLIDE ARM LIGHT TO ILLUMINATE. RE LAMPED SLIDE ARM LIGHT IAW MM 33-51-06-2-1, OPERATIONS CHECKED NORMAL.Feb 28, 2014 · N956FD · Boeing 757236 · Emergency LightingSDR CA140226004Duct · ruptured(CAN) UPON ENGINE START CREW OBSERVED LT BLEED LEAK EICAS MESSAGE. MAINTENANCE FOUND RUPTURED DUCT IN SECTION 48 FORWARD OF APU ISOLATION VALVE. THERE WAS EVIDENCE OF WEAR ON DUCT FROM HEAT SHIELD CLAMP AT RUPTURED AREA. DUCT REPLACED, SYSTEM CHECKED SERVIFeb 22, 2014 · Boeing 757236 · Pneumatic Distribution SystemSDR FDEA201402050271Girt Bar · dirtyL1 DOOR WOULD NOT LATCH, SLIDE & WOULD NOT ARM. REMOVED ICE & DEBRIS FROM DOOR SILL & FOUND GIRT BAR WOULD NOT DISARM PROPERLY. DOOR NOW OPERATES CHECKED GOOD & SHOWS PROPER LOCKING & UNLOCKING INDICATION. CLEANED GIRT BAR, ATTACH POINT & LUBED. CYCLED DOFeb 5, 2014 · N956FD · Boeing 757236 · Emergency EquipmentSDR FDEA201401260201Shear Tie · crackedFOUND SHEAR TIE CRACKED AT BS 1300 BETWEEN STRINGER 20 - 21L. REMOVED DAMAGED SHEAR TIE, FABRICATED NEW & INSTALLED IAW DWG 146N2002 REV EU & SRM 51-40-02.Jan 26, 2014 · N940FD · Boeing 757236 · Fuselage Internal Mounting StructureSDR FDEA201401150120Control Rod · bentR1 ARMING INDICATOR RETRACTABLE DOOR STICKY & HAS A WEAK SPRING. RELEASED FOR SERVICE IAW MEL 52-11-01-B. IDENTIFY L1 & OR R1 DOOR SLIDES, INOPERABLE OR MISSING. NO JUMP SEATER OR ACM ARE TO OCCUPY COURIER AREA IN FLIGHT. ARM INDICATOR RETRACTABLE DOOR CONJan 15, 2014 · N950FD · Boeing 757236 · Door Warning SystemSDR FDEA201401150106Fseu · malfunctionedLEADING EDGE SLAT ASYM ON TAKEOFF, OCCURRED AT WEIGHT OFF WHEELS ON TAKEOFF ROTATION. IAW AML 1565931 REPLACED NR 1 FSEU IAW MM 27-51-01-2. REPLACED RT INBD SLAT LOSS SWITCH IAW MM 27-81- 41-4. OPERATIONS CHECKED BAD, SUSPECT OUT OF ADJUSTMENT.Jan 15, 2014 · N630SH · Boeing 757236 · Trailing Edge Flap Control SystemSDR FDEA2014011400119Circuit Breaker · trippedDURING CLIMB OUT 20 MINS INTO FLIGHT, LT FWD BOOST PUMP CIRCUIT BREAKER TRIPPED.Jan 14, 2014 · N630SH · Boeing 757236 · Fuel Boost PumpSDR FDEA201312253040Light · inoperativeL1 SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-5-06-2-1. OPERATIONS CHECKED GOOD.Dec 25, 2013 · N978FD · Boeing 757236 · Emergency LightingSDR FDEA201312183001Fseu · inoperativeLEADING EDGE SLAT DISAGREE LIGHT ILLUMINATED DURING CONFIGURATION. FOLLOWED QRH, UNEVENTFUL LANDING. T/S PER FIM 27-81 FAULT TREE 803 FIG. 104 PG. 126 BLOCK 2, THE OVERLOAD INDICATOR WAS RESET. CHECKED ALL RIGHT WING ROTARY ACTUATORS PER MM 27-81-18 FIG 6,Dec 18, 2013 · N940FD · Boeing 757236 · Leading Edge Slat Control SystemSDR FDEA201312142983Unknown · malfunctionedPARKED AT GATE, SET PARKING BRAKE, PARKING BRAKE SHOWED ON EICAS. ACFT ROLLED FWD ANYWAY. SET PARKING BRAKE SEVERAL TIMES, FUNCTIONS NORMAL. PERFORMED ADJUSTMENT TEST IAW 757-200 MM 32-44-00-5. OPERATIONS CHECKED OK, NO HISTORY, OK FOR SERVICE.Dec 14, 2013 · N958FD · Boeing 757236 · Landing Gear Brake SystemSDR QPR2013F00000Slide · unwanted deployON ARRIVAL, MECHANIC OPENED L2 DOOR THAT HAD NOT BEEN DISARMED. DOOR SLIDE ACTIVATED AND DEPLOYED NORMAL.Dec 9, 2013 · N757SS · Boeing 757236 · Escape SlideSDR FDEA201311222854Relief Valve · faultyTEST FLIGHT OVER PRESS RELIEF VLV DID NOT OPEN UNTIL THE CABIN WAS AT 9.4 PSI. 757 FTAM SAYS VLV SHOULD OPEN BETWEEN 8.85 - 9.25. R & R UPPER PN 103642-3, SN 108-1297 & LOWER PN 103642-3 & SN 108-1263. POSITIVE PRESS RELIEF VLVS IAW B757 AMM 21-32-01-2. PNov 22, 2013 · N978FD · Boeing 757236 · Pressure Regulator/Outflow ValveSDR FDEA201311152792Bearing · brokenFOUND L1 DOOR HARD TO CLOSE. DISCOVERED BROKEN BEARING ON CRANK ROLLER IN UPPER CORNER. INSTALLED BEARING, DOOR OPERATES NORMAL.Nov 15, 2013 · N950FD · Boeing 757236 · Passenger/Crew DoorsSDR FDEA201311122742Skin · delaminatedRT SIDE EMPENNAGE, AFTER REMOVAL THE UPPER SKIN BETWEEN THE FWD SPAR AND FWD AUX SPAR FOUND DELAMINATION ON THE LOWER SKIN OF THE HONEYCOMB BETWEEN STABILIZER BS 176-224. REPAIRED IAW EA F-5510-T0303533. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Nov 12, 2013 · N979FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201311122734Structure · damagedRT SIDE OF EMPENNAGE AFTER REMOVAL THE UPPER SKIN BETWEEN THE FWD SPAR AND FWD AUX SPAR FOUND NUT PLATE HAS ELONGATED HOLE AT INBD LOGO LIGHT. REPAIRED IAW EA F-5510-T0303569. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Nov 12, 2013 · N979FD · Boeing 757236 · Horizontal Stabilizer StructureSDR FDEA201311122733Skin · delaminatedRT SIDE HONEYCOMB INTERIOR SIDE, LOWER SIDE OF UPPER SKIN, DELAMINATED. REMOVED AND REPAIRED OUT IAW EA F-5510-T0303533. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Nov 12, 2013 · N979FD · Boeing 757236 · Horizontal Stabilizer, Plate/SkinSDR FDEA201311122741Skin · delaminatedEMPENNAGE RT SIDE AFTER REMOVAL THE UPPER SKIN BETWEEN THE FORWARD SPAR AND FORWARD AUX SPAR FOUND DELAMINATION ON THE LOWER SKIN OF THE HONEYCOMB BETWEEN STABILIZER STA 128 -176. THE UPPER SKIN BETWEEN FORWARD SPAR AND FWD AUX SPAR ON THE LOWER SKIN BETWEEN Nov 12, 2013 · N979FD · Boeing 757236 · Horizontal Stabilizer, Plate/SkinSDR FDEA201311122740Skin · dentedDENT IN RT HORIZONTAL STABILIZER UPPER SURFACE BETWEEN FRONT SPAR AND REAR SPAR, STAB STA 200 -224. DENT REPAIRED IAW EAF-5510-T0303533. . REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 12, 2013 · N979FD · Boeing 757236 · Horizontal Stabilizer, Plate/SkinSDR FDEA201311122739Skin · distortedUPPER SKIN BETWEEN THE FORWARD SPAR AND FORWARD AUX SPAR FOUND HONEYCOMB HAS BEEN DISTORTED ON THE OTBD END AT STABILIZER STA 224. SKIN REPAIRED IAW EAF-5510-T0303533. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 12, 2013 · N979FD · Boeing 757236 · Horizontal Stabilizer, Plate/SkinSDR FDEA201311102723Bushing · migratedNR 2 PYLON LOWER SPAR FITTING BUSHING MIGRATED. REPAIRED PER SRM 54-50-90 REV 110 REPAIR 5. REPAIR CLASSIFIED AS MAJORNov 10, 2013 · N976FD · Boeing 757236 · Nacelle/Pylon, Main FrameSDR FDEA201311102721Skin · damagedNUMEROUS SMALL NICKS AND SCRATCHES BETWEEN STRINGER 26 RT AND 26 LT BS 620-640. DAMAGE REMOVED ANDFOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL II, REV 109 AND REPAIRED IAW EA F-5330-T0302663. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 10, 2013 · N979FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201311082715Skin · puncturedSKIN DENTED AT BS 460-480, STR 27L- 28L, PUNCTURED THROUGH. REPAIRED IAW EA F-5240-T0303070. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Nov 8, 2013 · N979FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201311082714Skin · damagedNUMEROUS SMALL NICKS AND SCRATCHES BETWEEN STRINGER 26 RT AND 26 LT AT BS 540-520, 540 -560, STR 26L-26R EXTERIOR SKIN NICKS AND SCRATCHES. REMOVED, FOUND OUT OF LIMIT AT STA 523, ABOVE STR 28L AND STA 529 BELOW STR 27L IAW SRM 53-00-01, FIG 101 DETAIL II, Nov 8, 2013 · N979FD · Boeing 757236 · Fuselage Main, Plate/SkinSDR FDEA201310312662Web · corrodedBS 1615 - 1620, S19R WEB TO STRINGER IS MISSING FIVE LOCK FASTENERS AND IS BULGING. CORROSION WAS OUT OF LIMITS IAW SRM 53-60-15, FIG 101, DET. 8, CAT "B". REPAIRED IAW 60000410860001, EA 757-5361-16-F4347, REV-.Oct 31, 2013 · N978FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201310302655Frame · corrodedNR 3 CARGO DOOR LOWER FRAME BETWEEN FWD CAVITY, INTERNAL SIDE CORRODED, REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-00-53, DET V, FIG 101. REMOVED DAMAGE AREA IAW SRM 51-70-13 FIG 1. INSTALLED REPAIR IAW SRM 51-40-02 AND 51-70-13, FIG Oct 30, 2013 · N978FD · Boeing 757236 · Cargo/Baggage DoorsSDR FDEA201310292644Girt Bar · looseL1 DOOR SLIDE WILL NOT DISARM. GIRT BAR REMAINS ENGAGED IN FWD FLOOR LOCK. SLIDE STOWED. FOUND GIRT LOOSE FROM DOOR. ATTACHED IAW MM 25-66-10-2. OPS CHECKED NORMAL.Oct 29, 2013 · N953FD · Boeing 757236 · Emergency EquipmentSDR FDEA201310292638Structure · corrodedLEFT INBD MAIN FLAP CORRODED. R & R LT INBD MAIN FLAP IAW AMM 27-51-02/401. ADJUSTED IAW AMM 27-51-02/501. PERFORMED TEST IAW AMM 27-51-02-5. CHECKED GOOD.Oct 29, 2013 · N978FD · Boeing 757236 · Trailing Edge FlapsSDR FDEA201310282630Web · corrodedFLOOR WEB CORRODED UPPER SURFACE LBL 12 BS 420-440. REMOVED CORROSION FROM WEB, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 5.4.3.Oct 28, 2013 · N951FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR FDEA201310272628Seat Track · corrodedSEAT TRACK SPLICE CORRODED, LBL 24, BS 420-440. REMOVED DAMAGED SEAT TRACK SPLICE. FABRICATED AND INSTALLED IAW DRAWINGS 3505,3475 REV G, AND 3458 REV K.Oct 27, 2013 · N951FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201310272627Floorbeam · chafedBS 1640 BL 0 - LBL 30, FLOORBEAM UPPER FLANGE FOUND CHAFED AROUND FASTENER HOLES. FLOORBEAM REMOVED IAW SRM 51-40-02 REVISION 109. NEW FABRICATED FLOORBEAM INSTALLED IAW DWG 146N5089 SHEET 1 REV B. REPAIR IS CLASSIFED MAJOR IAW GMM 6-2-100.Oct 27, 2013 · N979FD · Boeing 757236 · Fuselage Main, Floor Beam
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