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 RYN2008F00021Line · brokenPILOT REPORT LT ENGINE NOT MAKING POWER AT FL 20000 WITH THE ENGINE POWER LEVER FULLY FWD AND N1 WAS ONLY 71 PERCENT. REPLACED THE LT ENGINE P1 PROBE BROKEN SENSE LINE. COMPLIED WITH HIGH POWER ENGINE RUN, NO DEFECT NOTED. (K)Sep 10, 2008 · N526NA · Boeing 757236 · Indicating/Recording SystemSDR FDEA200808253579Skin · corrodedNR 2 PYLON INTERIOR SURFACE BETWEEN PANELS 443 AR AND 443 BR HAS LIGHT CORROSION. REMOVED AND REPLACED NR 2 PYLON OTBD SKIN PANEL PN 311N5046-32 IAW DWG 311N5002 AND SRM 51-40-02, CATEGORY A MAJOR REPAIR NO FOLLOW-UP TRACKING REQUIRED .Aug 25, 2008 · N915FD · Boeing 757236 · Nacelle/Pylon, Plate/SkinSDR FDEA200808253578Skin · corrodedNR 1 PYLON OTBD FWD 311N5193-1 SKIN PANEL HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED SKIN PAANEL IAW SRM 51-40-02, AND DWG 311N5002, 311N5108. (CATEGORY A MAJOR REPAIR, NO FOLLOW-UP TRACKING REQUIRED)Aug 25, 2008 · N915FD · Boeing 757236 · Nacelle/Pylon, Plate/SkinSDR 08FDEA03579Skin Panel · corrodedNR 2 PYLON INTERIOR SURFACE BETWEEN PANELS 443 AR AND 443 BR HAS LIGHT CORROSION. REMOVED AND REPLACED NR 2 PYLON O/B SKIN PANEL P/N 311N5046-32 IAW DWG 311N5002 AND SRM 51-40-02, CATEGORY A MAJOR REPAIR NO FOLLOW-UP TRACKING REQUIRED .Aug 25, 2008 · N915FD · Boeing 757236 · Nacelle/Pylon, Plate/SkinSDR 08FDEA03578Skin Panel · corrodedNR 1 PYLON O/B FWD 311N5193-1 SKIN PANEL HAS CORROSION ON INNER SURFACE. REMOVED AND REPLACED SKIN PANEL IAW SRM 51-40-02,AND DWG. 311N5002, 311N5108, CATEGORY A MAJOR REPAIR, NO FOLLOW-UP TRACKING REQUIRED.Aug 25, 2008 · N915FD · Boeing 757236 · Nacelle/Pylon, Plate/SkinSDR FDEA200808143427Seat Track · damagedUPON REMOVAL OF SEAT TRACK AT LBL 24, BS 540-640, MAIN CABIN, IT WAS DISCOVERED THAT THERE WERE SEVERAL EXISTING ELONGATED FASTENER HOLES. TWO EACH AT BS 540-620 AND ONE EACH ON THE FOWARD SIDE OF BS 640. REPAIRED SEAT TRACK PER MAE EA 757-5335-16-F0975,Aug 14, 2008 · N906FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA03426Skin · corrodedLT WING REAR SPAR UPPER FITTING, UPPER SKIN LOWER SURFACE, ALONG THE AFT EDGE WHERE SKIN OVERLAPS THE REAR SPAR'S UPPER CAP, IS CORRODED JUST ABOVE LT DEFUEL VALVE. REPAIRED WING PANEL IAW FEDEX EA F-5730-110881, REV -, DATED 06/19/2008 AND SB 757-57- 0036, Aug 14, 2008 · N915FD · Boeing 757236 · Wing, Plate/SkinSDR 08FDEA03425Seat Track · corrodedSEAT TRACK LBL 45.50 HAS CORROSION ON AFT SIDE OF BS 1120 FLOORBEAM. REMOVED CORROSION FROM SEAT TRACK IAW SRM 53-00-52. ORIGINAL MATERIAL THICKNESS WAS .084 INCH, AFTER REWORK .044 INCH. FOUND TO BE OUT OF LIMITS PER SRM 53-00-52. REMOVED SEAT TRACK, FABRAug 14, 2008 · N915FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200808073308Crease Beam · corrodedMAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. REMOVED CORROSION IAW SRM 51-10-02. L=VARIOUS AREAS TOTAL 6.5 INCHES, W=1.5 INCH, D=0.035 INCH. FOUND TO BE OUT OF LIMITS NO SRM REFERENCE. Aug 7, 2008 · N915FD · Boeing 757236 · Fuselage Main, KeelSDR FDEA200808073307Crease Beam · corrodedMAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. REMOVED CORROSION IAW SRM 51-10-02. L=VARIOUS AREAS TOTAL 6.5 INCHES, W=1.5 INCHES, D=0.035 INCH. FOUND TO BE OUT OF LIMITS NO SRM REFERENCAug 7, 2008 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR FDEA200808073306Floor Support · corrodedMAIN CABIN FIXED FLOOR STRUCTURE BETWEEN STA 1681.8-1720 HAS SEVERAL AREAS OF CORROSION. BLEND CORROSION IAW SRM 51-10-02, AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51. FABRICATED REPAIR DOUBLERS IAW SRM 53-60-51 FRON 2024-T3 .063 BATCH NR 0001466849. IAug 7, 2008 · N915FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR 08FDEA03308Crease Beam · corrodedMAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. REMOVED CORROSION IAW SRM 51-10-02, L=VARIOUS AREAS TOTAL 6.5'', W=1.5'', D=0.035. FOUND TO BE OUT OF LIMITS NO SRM REFERENCE. REMOVED CREAAug 7, 2008 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR 08FDEA03307Crease Beam · corrodedMAIN CABIN, CREASE BEAM INBD CHORD BS 395-BS 418 LBL 65 HAS CORROSION ALSO SEE BS 331 AT FASTENER HOLE FOR CORROSION. REMOVED CORROSION IAW SRM 51-10-02, L=VARIOUS AREAS TOTAL 6.5'', W=1.5'', D=0.035. FOUND TO BE OUT OF LIMITS NO SRM REFERENCE. REMOVED CREAAug 7, 2008 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR 08FDEA03306Web · corrodedMAIN CABIN FIXED FLOOR STRUCTURE BETWEEN STA 1681.8-1720 HAS SEVERAL AREAS OF CORROSION. BLEND CORROSION IAW SRM 51-10-02, AREAS FOUND TO BE OUT OF LIMITS IAW SRM 53-60-51 PG FIG. FABRICATED REPAIR DOUBLERS IAW SRM 53-60-51. INSTALLED REPAIR DOUBLERS IAW SRAug 7, 2008 · N915FD · Boeing 757236 · Fuselage Miscellaneous StructureSDR RYN2008F00011Windshield · crackedACFT RETURNED TO BUD. FLIGHT CREW ADVISED THAT THE LT NR 1 WINDSHIELD IS CRACKED ALONG THE LOWER SECTON OF THE WINDOW. WAITING FOR PARTS. OPEN. (S)Aug 6, 2008 · N526NA · Boeing 757236 · Flight Compartment WindowsSDR RYN2008F00009Windshield · crackedLEFT NR 1 WINDSHIELD CRACKED. REPLACED LEFT NR 1 WINDSHIELD AND WINDOW HEAT CONTROLLER IAW AMM 56-11-01 AND AMM 50-41-01 OPS CHECKED NORMAL. (A)Jul 23, 2008 · N526NA · Boeing 757236 · Flight Compartment WindowsSDR 08FDEA02875Seat Track · damagedSTA 1046, LBL 47, LUG SCALLOP IS MISSING ON SEAT TRACK. REMOVED SEAT TRACK SECTION IAW SRM 53-00-52. FABRICATED NEW ON MAE TRAV NR T8/750424. INSTALLED NEW SEAT TRACK REPAIR PARTS IAW SRM 51-40-02, AND 53-00-52.Jul 14, 2008 · N915FD · Boeing 757236 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA02874Crease Beam · corrodedMAIN CABIN CREASE BEAM CHORD BS 680 -740, RBL 66 HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CREASE BEAM, RECEIVED NEW PART NR 143N8328U54 IAW SRM 53-30-13. INSTALLED NEW CREASE BEAM PART IAW SRM 51-40-02, AND 51-10-02, FS 680-740, RJul 14, 2008 · N915FD · Boeing 757236 · Fuselage Main, StructureSDR ANC2008F00000Unknown · unknownPILOT REPORT 4274013-1: DURING SINGLE ENG TAXI WHILE APPLYING THRUST RT ENGINE STALLED THEN AFTER THE LT ENG WAS STARTED, IT ALSO STALLED LT ENG LIMITER COME ON AT THE EICAS. LT BVCU SHOWS CODE 07, IAW FIM 75-32-00 TABLE 102 GEN DEDICATED CONTROL UNIT "B" WASJul 12, 2008 · N521NA · Boeing 757236 · Standard Practices/StructuresSDR 08FDEA02690Floorbeam · corrodedMAIN CABIN FLOOR STA 365 RBL 58 FLOORBEAM CORROSION. REMOVED DAMAGE, FABRICATED ANGLES MAE TRAV T8/748437. FABRICATED T-CHORDS MAE TRAV T8/748430, IAW SRM 53-00-51. INSTALLED REPAIR PARTS STA 365 RBL 34-70 IAW SRM 53-00-51 FIG 201. REPAIR 3. MAJOR REPAIJul 3, 2008 · N915FD · Boeing 757236 · Fuselage Main, Floor BeamSDR RYN2008F00000Computer · malfunctionedAIR TURN BACK, DUE TO LOSS OF ALL 3 AUTO PILOTS AND THE CAPTAIN`S FLIGHT DIRECTOR, COULD NOT ENTER RVSM AIRSPACE. RESET LT FCC AND ACCOMPLISHED TEST 2 AND 10 IAW AMM 22-30-00. ALL CHECKED NORMAL. (K)Jul 1, 2008 · N526NA · Boeing 757236 · Flight Management Computing Hardware SystemSDR RYN2008F00004Control Panel · malfunctionedAIR TURNBACK TO RFD FOR PRESSURE CONTROLLER PROBLEM, BOTH AUTO 1 AND AUTO 2 ARE SPIKING 200 TO 300 CABIN DIFFERENTIAL DURING CLIMB. REPLACED OVERHEAD CONTROL PANEL IAW AMM 21-31-01, OPS CHECKED NORMAL. IN ADDITION COMPLIED WITH FIM 21-30-00 AND AMM 21-30-00 Jun 27, 2008 · N526NA · Boeing 757236 · Cabin Pressure Control SystemSDR 08FDEA02463Floorbeam · corrodedMAIN CABIN BS 418, BL0 TO LBL 15, FLOORBEAM HAS AREAS OF CORROSION AROUND FASTENER HOLES. CLEANED AREA AND CHECKED LIMITS IAW SRM 51-10-3 AND 53-00-51, DETAIL 3. FLOORBEAM OUT OF LIMITS PER SRM 53-00-51, DETAIL 3; ORIGINAL MATERIAL THICKNESS .125 INCH, AFTJun 25, 2008 · N915FD · Boeing 757236 · Fuselage Main, Floor BeamSDR 08FDEA02432Floorbeam · corrodedMAIN CABIN FLOORBEAM STA 1640 RBL 47-51 HAS CORROSION BLENDED AREA IAW SRM 51-10-02, ORIG MAT. .125 AFTER 0.90 FOUND OUT LIMITS, IAW SRM 53-00-51 PAGE 103, CUT OUT DAMAGED AREA STA 1640 BET RBL36.5 TO RBL 68.5, IAW SRM 53-00-51 PAGE 201. RECEIVED REPAIR PARTSJun 24, 2008 · N915FD · Boeing 757236 · Fuselage Main, Floor BeamSDR 08FDEA02431Floorbeam · corrodedSTA 377.7, BL0 TO LBL 45 HAS CORROSION AROUND NUT PLATE HOLES. REMOVED DAMAGED AREA, LBL 13 TO LBL 70, BS 377.7 IAW SRM 53-00-51, FIG 201, REPAIR NR 3. FABRICATED T-CHORD AND SHIM IAW SRM 53-00-51, REPAIR NR 3. FABRICATED STRAP NR 4 AND NR 5 ON TRAVELER NR Jun 24, 2008 · N915FD · Boeing 757236 · Fuselage Main, Floor BeamSDR RYN2008F00005Structure · damagedREPAIR SECTION 48 TAIL SKID DAMAGE. REPAIRED SECTION 48 IAW 6-1171-RE-01647.Jun 20, 2008 · N526NA · Boeing 757236 · Fuselage Main, StructureSDR 08FDEA01868Skin · dentedR1 DOOR SKIN DENTED. REMOVED DAMAGE AND INSTALLED A DOUBLER REPAIR ON R1 DOOR SKIN IAW SRM 52-10-01 REPAIR NR 2, FIGURE 202. THIS REPAIR IS CLASSIFIED AS A "MAJOR" REPAIR, CATEGORY A, WITH NO FOLLOW UP TRACKING REQUIRED.May 16, 2008 · N915FD · Boeing 757236 · Cargo/Baggage DoorsSDR ANCF200800009Cable · overheatedWINDOW HEAT CABLES OF L SIDE WINDOW OVERHEATED PRODUCING FUMES L SIDE WINDOW HEAT SW WAS TURNED OFF. DEFERRED TO DMI LOG BOOK ITEM NR 307 WAS INSPECTED L SIDE WINDOW POWER LINES AND FOUND BURNT. DUE THIS CONDITION L SIDE WINDOW HEATING IS DEACTIVATED AND DEFMay 5, 2008 · N521NA · Boeing 757236 · Ice/Rain Protection System WiringSDR ANCF200800006Duct · damagedENG OVHT DISPLAYED WITH ENG OVHT LIGHT ILLUM. LIGHT EXTING AFTER THRUST REDUCTION AND CAUTION LIGHT ON. 4AW AMM 36-11-01 P.401 / 36-11-07 P.401. REMOVED AND REPLACED BOTH HP2 AND HP6 DUCT ASSY IAW AMM 71-00-00 ENG RUN PERFORMED SATISFACTORY. P/N 312N5306-1 Mar 23, 2008 · N522NA · Boeing 757236 · Pneumatic Distribution SystemSDR ANCF200800005Unknown · unknownDURING CLIMB, 8 MINUTES AFTER TAKEOFF, AT 20.500 FEET, EICAS MESSAGE "LEFT ENGINE OVERHEAT" IS SHOWED. CHECK LIST WAS PERFORMED. VISUAL INSPECTION AND CHECK OF CONDITION OF ALL PNEUMATIC DUCTS, VALVES AND ALSO LINES. BITE PROCEDURE WAS ACCOMPLISHED IN ACCORJan 3, 2008 · N522NA · Boeing 757236 · Central WarningSDR ANCF200700031Connector · damagedAFTER TAKEOFF, GEN OFF EICAS MESSAGE WAS PRESENTED. ALSO LEFT BUSS ISOLATED MESSAGE WAS PRESENTED AND SEVERAL CAPTAIN INSTRUMENTS WERE LOST. THERE WAS NOT FLIGHT INSTRUMENT TRANSFER AND THE AUTOPILOT AUTOMATICALLY DISCONNECTED. GEN OFF CHECK LIST WAS ACCOMPDec 10, 2007 · N506NA · Boeing 757236 · Electrical Power System WiringSDR ANCF200700029Blades · damagedN1 ENGINE VIBRATION HIGH, READS 3.0. ENGINE INDICATIONS NORMAL. VIBRATION RETUNED BELOW 2.5 WITH THRUST LEVER RETARDED. ENGINE WAS NOT SHUTDOWN. ON THE LT ENGINE FAN BLADE NR 17 WAS REPLACED CHOCKING PAD IAW AMM 72-31-73 PAGE 401, IAW AMM 71-00-00 PAGE 548, Nov 14, 2007 · N521NA · Boeing 757236 · Turbine Engine Compressor SectionSDR ANCF200700028Filter · crackedPILOT REPORT: AIRPLANE RETURN TO RAMP DUE TO TECHNICAL PROBLEMS ( HYD SYS QTY). DURING INSPECTION FOUND THE POWER TRANSFER UNIT PRESSURE FILTER MODULE WITH LEAKAGE. REMOVED AND REPLACED THE PTU PRESSURE FILTER MODULE IAW AMM 29-22-02 PAGE 401. OPS TEST OK.Oct 29, 2007 · N521NA · Boeing 757236 · Hydraulic Filter, AuxiliarySDR ANCF200700026Unknown · unknownBOG 13L. DURING ROLLING TAKEOFF, THE NOSE WHEEL STEERING GOT STUCK AND THEN THE TAKEOFF WAS REJECTED, THE AIRPLANE WENT TO THE RT, OUT OFF THE RUNWAY WITHOUT CONTROL. IN PROCCESS; THE SYSTEMS AND SUB-SYSTEMS ARE BEING CHECKED AND INSPECTED BY TROUBLESHOOTING Oct 25, 2007 · N521NA · Boeing 757236 · Landing Gear Steering SystemSDR ANCF200700025Control Panel · malfunctionedA/T FAILED TO ENGAGE WHEN EPR MODE SELECTED ON T/O THE EPR SW DID NOT ENGAGE. THE T/O WAS DISCONNECTED, IAW MCC THE PROCEDURE FOR T/O WILL PERFORM MANUALLY A SECOND ATTEMPT WAS MADE AND THE TIME TO ENGAGE THE AUTOPILOT INFLIGHT DID NOT ENGAGE L,C OR R. IAWOct 19, 2007 · N521NA · Boeing 757236 · Autopilot SystemSDR ANCF200700019Fire Loop · malfunctionedPILOT REPORT: RT ENGINE FIRE AT MDE THE FAULT WAS PRESENTED AFTER 5 MIN OF DEPARTURE. BOTTLE NR 1 WAS DISCHARGED AND RETURNED TO MDE WITH NORMAL LANDING FLIGHT TIME WITH SINGLE ENG +/- 13 MTS. INSPECTED RT ENGINE IAW AMM 71-00-00 PAGE 604. NO FIRE EVIDENCE FOJul 26, 2007 · N522NA · Boeing 757236 · Smoke DetectionSDR ANCF200700014Tube · malfunctionedDURING CRUISE AT FL 370 A DIFFERENCE BETWEEN BOTH ENGINE FUEL FLOWS WAS DETECTED WHILE THE OTHER ENGINE PARAMETERS WERE NORMAL LITTLE BY LITTLE THE FF DIFFERENCE WAS INCREASING UNTIL LEFT FF 5686 AND RIGHT FF 2678. THE AIRSPEED WAS AFFECTED BY THIS CONDITION Jun 11, 2007 · N521NA · Boeing 757236 · Fuel Flow IndicatingSDR ANCF200700011Motor · inoperativeFLAPS FAIL TO MOVE, TRAILING EDGE LIGHT ILLUMINATED AND AICES MSG TE FLAPS DISAGREE AND FLAP ISLN VAL DISPLAYED. FLAPS OPERATE NORMAL USING TE ALTN SYSTEM. FLAP LEVEL VIBRATION WAS FELT DURING OPERATION WHEN TAXING OUT. IN ACCORDANCE WITH FIM 27-51-00 FIG 1May 29, 2007 · N506NA · Boeing 757236 · Hydraulic System, MainSDR CA070504001Line · leaking(CAN) FORWARD PYLON PRESSURE LINE FOUND CHAFED THROUGH CAUSING LEAK. DAMAGE CAUSED BY A DEFECTIVE HOSE CLAMP. (TC NR 20070504001)May 1, 2007 · Boeing 757236 · Nacelle/Pylon StructureSDR PIDA07018Battery Pack · dischargedEMERGENCY LIGHTS IN VICINITY OF THE L2 DOOR ARE INOP. REPLACED BATTERY PACK AND OPS CHECKED OK.Apr 13, 2007 · N757BJ · Boeing 757236 · Emergency LightingSDR PIDA07015Keelbeam · corrodedDURING INSPECTION, CORROSION WAS FOUND ON THE RIGHT KEEL BEAM HORIZONTAL LEG UPPER SURFACE BETWEEN BS 1146 AND BS 1154 IN THE RIGHT MLG WHEEL WELL. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH EA 53-069 DATED 03/11/07 WITH FAA DER APPROVED 8110-3 DATED MARCH 11Mar 14, 2007 · N757BJ · Boeing 757236 · Fuselage Main, KeelSDR PIDA07014Skin · dentedDURING INSPECTION, A DENT WAS FOUND IN THE FUSELAGE SKIN AT BS 1620 JUST ABOVE STR 17LT. DENT REPAIRED IN ACCORDANCE WITH BOEING MESSAGE 1-295219323-1, -4, -5, -7, -8, AND -9 WITH FAA DOA APPROVED 8100-9 DATED 13 MARCH 2007.Mar 9, 2007 · N757BJ · Boeing 757236 · Fuselage Main, Plate/SkinSDR PIDA07013Fairing · damagedDURING INSPECTION, FOUND CORROSION ON LOWER SURFACE OF LEFT WING AT THE FORWARD ATTACH POINT FOR THE I/B FLAP TRACK FAIRING (WING STA 285.65). REPAIRED PER BOEING MESSAGES 1-281963543-1 AND 1-281963543-9 WITH FAA DOA APPROVED 8100-9 DATED 3-6-2007.Mar 9, 2007 · N757BJ · Boeing 757236 · Trailing Edge FlapsSDR PIDA07010Skin · delaminatedDURING INSPECTION FOUND LEADING EDGE OF LEFT WING AT THE NR 5 SLAT DELAMINATED SIX INCHES FROM THE OUTBOARD END ON THE UPPER SURFACE. REPAIRED AREA PER SRM 57-41-01 AND SRM 51-70-17 WITH MINOR DEVIATIONS PER EA 57-046.Mar 5, 2007 · N757BJ · Boeing 757236 · Leading Edge DevicesSDR PIDA07011Skin · corrodedDURING INSPECTION FOUND THE LEFT WING NR 2 SLAT LOWER SURFACE HAS CORROSION 46 INCHES FROM THE INBOARD END. REPAIRED AREA PER EA 57-032.Mar 5, 2007 · N757BJ · Boeing 757236 · Leading Edge DevicesSDR CA070227002Drive Unit · burned(CAN) WXR RADAR DRIVE UNIT FOUND WITH TERMINAL 15 AND 16 BURNED (TC NR 20070227002)Feb 25, 2007 · Boeing 757236 · Weather Radar SystemSDR CA070226001Connector · burned(CAN) CREW REPORTED EICAS STATUS MESSAGE, WXR SYSTEM. ON REPLACEMENT OF WXR DRIVE UNIT, FOUND BURNED ELECTRICAL CONNECTORS. (TC NR 20070226001)Feb 21, 2007 · Boeing 757236 · Navigation System WiringSDR PIDA07012Frame · corrodedDURING INSPECTION FOUND CORROSION ON AN INTERNAL FRAME WEB ON THE FORWARD SIDE OF THE L4 DOOR WINDOW. CUT INNER SKIN OF DOOR FOR ACCESS AND REPLACED DAMAGED FRAME SECTION PER SRM 51-70-11 FIGURE 1 AND DWG 146N6100 AND REPAIRED INNER DOOR SKIN PER EA 52-031.Feb 19, 2007 · N757BJ · Boeing 757236 · Service DoorsSDR PIDA07009Pan · corrodedFORWARD LAVATORY SERVICE DOOR PAN AND SURROUNDING STRUCTURE CORRODED. REPLACED PAN AND SURROUNDING STRUCTURE PER DRAWING 141N8631 AND SRM 51-40-02.Feb 12, 2007 · N757BJ · Boeing 757236 · Fuselage Miscellaneous StructureSDR PIDA07008Door Frame · dentedNUMBER 2 (AFT CARGO) DOOR HAS A DENT ON THE LOWER DOOR FRAME. REPLACED LOWER BEAM PER SRM 51-40-02 AND 51-10-02.Feb 8, 2007 · N757BJ · Boeing 757236 · Cargo/Baggage Doors
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