Boeing 757-222

Service difficulty reports · 15,539

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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 = '757222'
  ORDER BY difficulty_date DESC"

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SDR FDEA201601150168Gust Lock · crackedDURING SERVICE CHECK FOUND L1 DOOR HOLD, OPEN LOCK CRACKED. R & R L1 DOOR GUST LOCK IAW AMM 52-11-08-8. OPERATIONS NORMAL. ACFT IS OK FOR SERVICE.Jan 15, 2016 · N775FD · Boeing 757222 · Passenger/Crew DoorsSDR FDEA201601090092Crease Beam · corrodedCABIN STATION 960 - 984 RT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 116. REWORKED AREA, MEASURED ORIGINAL THICKNESS 0.063", REMAINING THICKNESS 0.053", MATERIAL REMOVED 0.010", FOUND OUT OF 10% LIMIT IAW SRM 53-40-13 FIG 101 ALJan 9, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601080090Stringer · dentedSTATION 430, STRINGER 18R, AFTER REMOVAL OF SKIN REPAIR, FOUND STRINGER DENTED. EVALUATED DENT IN STRINGER, FOUND NO ALLOWABLE DAMAGE FOR S/F ACFT. R & R STRINGER, STATION 395 - 439, STRINGER 18R IAW SRM 51-40-02. CAT A MAJOR REPAIR.Jan 8, 2016 · N791FD · Boeing 757222 · Fuselage Main, Longeron/StringerSDR FDEA201601080080Door Sill · damagedBS 360, R1 DOOR CUT OUT LOWER SILL WEB, FOUND ONE ELONGATED FASTENER HOLE. REPAIRED IAW DWG 141N8422 SHT 1 REV R. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Jan 8, 2016 · N778FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201601070072Splice · corrodedBS 1140 LT, CREASE BEAM INNER CHORD SPLICE FITTING, FOUND CORRODED. REMOVED IAW SRM 51-10-02 REV 116 & FOUND CORROSION MORE THAN 50% THROUGH. CREASE BEAM, INNER CHORD SPLICE FITTING REMOVED IAW SRM 51-40-02 REV 116. NEW CREASE BEAM, INNER CHORD SPLICE FITTIJan 7, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601060063Skin · gougedRIGHT WING INBD TOP FLAP, TOP SIDE HAS GOUGE & POSSIBLE CRACK IN SKIN. REPAIRED RT WING INBD TOP FLAP, TOP SKIN SURFACE IAW-SRM-51-70-07 CAT A MAJOR REPAIR, REF EA F-5750-T0322458 PT 1.Jan 6, 2016 · N791FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201601060062Skin · gougedRIGHT WING INBD TOP FLAP, TOP SIDE HAS GOUGE & POSSIBLE CRACK IN SKIN.Jan 6, 2016 · N791FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201601050032Skin · wornEMPENNAGE, LT SIDE, THE HORIZONTAL STABILIZER BLADE SEAL PERIMETER HAS WEAR AT BS 1862 - 1875, ABOVE STRINGER 17. CHAFE REMOVED, FOUND OUT OF LIMIT IAW SRM 53-80-01 FIG 101 DETAIL VII REV 116. REPAIR CARRIED OUT IAW SRM 53-80-01-2R FIG 201 DETAIL II REV 117.Jan 5, 2016 · N778FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201601040019Fitting · crackedBS 1140 RT, CREASE BEAM INNER CHORD SPLICE, FITTING FOUND CRACKED. REMOVED IAW SRM 51-40-02 REV 116. NEW SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 01 REV. INSTALLED IAW DWG 144N5200 SHT 01 REV B. REPAIR CLASSIFIED AS MAJOR.Jan 4, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601040018Fitting · corrodedBS 1120 LT, CREASE BEAM INNER CHORD SPLICE, FITTING FOUND CRACKED & CORRODED. REMOVED IAW SRM 51-40-02 REV 116. NEW SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 01 REV. INSTALLED IAW DWG 144N5200 SHT 01 REV B. REPAIR CLASSIFIED AS MAJOR.Jan 4, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601040017Fitting · corrodedBS 1080 LT, CREASE BEAM INNER CHORD SPLICE, FITTING FOUND CRACKED & CORRODED. REMOVED IAW SRM 51-40-02 REV 116. NEW SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 01 REV. INSTALLED IAW DWG 144N5200 SHT 01 REV B. REPAIR CLASSIFIED AS MAJOR.Jan 4, 2016 · N778FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201601040016Fitting · corrodedBS 1120 RT, CREASE BEAM INNER CHORD SPLICE, FITTING FOUND CORRODED. REMOVED IAW SRM 51-10-02 REV 116. NEW SPLICE FITTING FABRICATED IAW DWG 144N5215 SHT 01 REV. INSTALLED IAW DWG 144N5200 SHT 01 REV B. REPAIR CLASSIFIED AS MAJOR.Jan 4, 2016 · N778FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201601040015Crease Beam · corrodedBS 940 - 960 LT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 116. EVALUATION CARRIED OUT ORIGINAL THICKNESS 0.056", REMAINING THICKNESS 0.034", FOUND OUT OF 10% LIMIT IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMJan 4, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601040014Crease Beam · corrodedBS 1100 - 1120 LT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 116. EVALUATION CARRIED OUT, ORIGINAL THICKNESS 0.063", REMAINING THICKNESS 0.055", FOUND OUT OF 10% LIMITS IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEBJan 4, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601040013Crease Beam · corrodedBS 1080 - 1100 LT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 116. EVALUATION CARRIED OUT, ORIGINAL THICKNESS 0.071", REMAINING THICKNESS 0.060", FOUND OUT OF 10% LIMITS IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEBJan 4, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201601040012Crease Beam · corrodedBS 960 - 984 , LEFT CREASE BEAM WEB FOUND CORRODED. FOUND OUT OF LIMITS IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. REMOVED AND REPLACED IAW SRM 51-40-02 REV 116, AND DWG 144N5140 SHT 03 REV D. REPAIR CLASSIFIED AS MAJOR.Jan 4, 2016 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201512314109Floor Support · crackedCOCKPIT BS 200 - 205, RBL 35 - RBL 38, FLOOR SUPPORT FOUND CRACKED. REMOVED AND REPLACED IAW SRM 51-40-02 REV 116, AND DWG 141N5810 SHEET 1 REV G. REPAIR CLASSIFIED AS MAJOR.Dec 31, 2015 · N778FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201512304107Skin · dentedINCOMING FUSELAGE SKIN DENT, BS 467, STRINGER 19R, DENT WAS FOUND OUT OF LIMITS DUE TO PROXIMITY TO THE LAP JOINT FASTENER LOCATIONS. ACCOMPLISHED EA F-5330-T0322263 PT 1 DATED DEC 15 2015. FUSELAGE PLATES & SKINS, DENT & GOUGE REWORKED. THIS IS A CAT B RDec 30, 2015 · N791FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201512294100Seat Track · damagedBS 608, RBL 45.5, SEAT TRACK INNER FLANGE, FOUND ONE ELONGATED HOLE. REPAIRED IAW EA F-5310-T0321333. REPAIR CLASSIFIED AS MAJOR.Dec 29, 2015 · N777FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR IXXA20151230120Switch · dirtyEICAS MSG DISPLAYED STEADY. LT FWD ENTRY DOOR OPEN. LIGHT DID NOT DISPLAY. INSPECTED & CHECKED LT FWD ENTRY DOOR LATCHING & INDICATION. CLEANED & LUBED DOOR LATCH SWITCH PLUNGER. NR 1 ENTRY DOOR & ADJUSTMENT TEST SYS SATISFACTORY. OPERATIONS CHECKED SATIDec 29, 2015 · N531UA · Boeing 757222 · Door Warning SystemSDR FDEA201512284088Support Angle · corrodedBS 1681, R4 DOOR SCUFF PLATE SUPPORT ANGLE FOUND CORRODED. REPAIRED IAW EA F-5310-T0321518 PART 1. REPAIR CLASSIFIED AS MAJOR.Dec 28, 2015 · N777FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201512284098Door Sill · corrodedBS 680 - 730, R2 DOOR CUT OUT LOWER SILL INNER CHORD FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 116. EVALUATION CARRIED OUT, ORIGINAL THICKNESS 0.080", REMAINING THICKNESS 0.069", FOUND OUT OF 10% LIMITS IAW SRM 53-30-15 ALLOWABLE DAMAGE 1 REV 11Dec 28, 2015 · N778FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201512284097Crease Beam · corrodedCABIN STATION 1140 - 1160, LT CREASE BEAM WEB FOUND CORROSION. CREASE BEAM REMOVED AS PER SRM 51-10-02 REV 116. ORIGINAL THICKNESS 0.063" REMAINING THICKNESS 0.054". FOUND OUT OF 10% LIMIT AS PER SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMODec 28, 2015 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201512284096Crease Beam · corrodedCABIN STATION 1140 - 1160, RT CREASE BEAM WEB FOUND CORROSION. CORROSION REMOVED IAW SRM 51-10-02 REV 116. ORIGINAL THICKNESS 0.063", REMAINING THICKNESS 0.053", FOUND OUT OF 10% LIMITS IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 REV 116. CREASE BEAM WEB REMOVED IADec 28, 2015 · N778FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201512284095Seat Track · chafedBS 1165 - 1170, RBL 45.5, SEAT TRACK FOUND CHAFED. REMOVED & FOUND OUT OF LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 REV 116, MEASURED LIP DISTANCE 0.49". SEAT TRACK, BETWEEN STATION 1075 - 1180, RBL 45.5 R & R WITH NEWLY FABRICATED SEAT TRACK IAW DWG 144N50Dec 28, 2015 · N778FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201512284094Seat Track · chafedCABIN STATION 1165 - 1170, RBL 24.75, SEAT TRACK CROWN FOUND CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 116. FOUND OUT OF LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 REV 116. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-02 REV 116, DWG 144N5021 SHT 1 REV A,Dec 28, 2015 · N778FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201512284093Seat Track · chafedBS 1165 -1170, LBL 24.75 SEAT TRACK CROWN FOUND CHAFED. CHAFE REMOVED IAW SRM 51-10-02 REV 116. FOUND OUT OF LIMITS IAW SRM 53-00-52 ALLOWABLE DAMAGE 1 REV 116. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-02 REV 116, DWG 144N5021 SHT 1 REV A, AND DWG 144Dec 28, 2015 · N778FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201512284092Seat Track · chafedCABIN STATION 1180 - 1200, LBL 45.5 SEAT TRACK CROWN CHAFED. COMPLIED WITH EA F-5310-T0323360 A PART 1. OUT OF LIMIT CHAFED MARK FOUND ON SEAT TRACK LIP CROWN, AT STATION 1198, LBL 45.50. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Dec 28, 2015 · N778FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201512284091Seat Track · chafedCABIN STATION 982 - 990, RBL 24.75 SEAT TRACK CROWN FOUND CHAFED. SEAT TRACK CROWN REMOVED AS PER SRM 51-10-02 REV 116. EVALUATION CARRIED OUT REMAINING DIMENSION 0.17" AND FOUND OUT OF 0.26" LIMIT PER SRM 53-00-52 ALLOWABLE DAMAGE 1 REV 116. SEAT TRACK CRODec 28, 2015 · N778FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201512244076Fire Detector · false activationMAIN CARGO FIRE WARNING SYS ACTIVATED ON LANDING. SUSPECT DUST INTAKE FROM RNWY. IAW CREW DEBRIEF, AFTER DUST CLEARED, MAIN CARGO SMOKE DETECTION CLEARED. PERFORMED MAIN CARGO SMOKE DETECTION TEST IAW MM 26-16-30-5. SYS TESTED NORMAL. ACFT OK FOR SERVICE.Dec 24, 2015 · N770FD · Boeing 757222 · Fire DetectionSDR FDEA201512244075Door Frame · crackedPASSENGER DOORS, CRACK NOTED ON NR 2R, PAX DOOR INNER CHORD OF THE DOOR FRAME AT THE UPPER HINGE CUT OUT. REPAIRED R2 DOOR FWD FRAME IAW SRM 52-10-02-2R REPAIR 1, REPAIR CLASSIFIED AS A CAT B MAJOR REPAIR. COMPLIED WITH EA F-5210-T0322556 PT 1 RELEASE DATE ODec 24, 2015 · N791FD · Boeing 757222 · Passenger/Crew DoorsSDR CALA2015122494917Warning System · false activationLEADING EDGE SLAT DISAGREE. EMER DECLARED WITH ATC IAW FIM. OPERATED SLATS SEVERAL CYCLES WITH NORMAL HYD OPERATIONS & ALTERNATE ELEC LE SLAT MOVE FREELY & NO ECAS MSG NOTED. CHECKED PDU FOR LEAKS, NO LEAKS NOTED. PERFORMED FSEU BITE PROCEDURE IAW FIM, NO Dec 23, 2015 · N595UA · Boeing 757222 · Leading Edge Slat Position Indicating SystemSDR FDEA201512184027Longeron · dentedAFTER REMOVAL OF EXISTING SKIN REPAIR, STATION 1725, STRINGER 17L, FOUND DENT IN LONGERON. R & R LONGERON, LOWER CHORD IAW SRM-51-40-02. CAT A MAJOR REPAIR. FABRICATED ON T15 1171504 & DWG 145N9202-5.Dec 18, 2015 · N791FD · Boeing 757222 · Fuselage Main, Longeron/StringerSDR FDEA201512164019Skin Panel · corrodedPITTING CORROSION AT LAP SEAM, STRINGER 19R, BS 740 - 760. ACCOMPLISHED EA F5330-T0322184, PART 1 FUSELAGE PLATES & SKINS CORROSION REWORK. THIS IS A CAT B REPAIR. REF FORM 8110-3 DATED 12 08 2015. MAJOR REPAIR.Dec 16, 2015 · N791FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR CALA2015121794907Skin · corrodedEXISTING AFT FUSELAGE BELLY DOUBLER, BETWEEN BS 1701 TO 1720, JUST AFT OF AFT LAVATORY SERVICE PAN, HAS ONLY 2 ROWS OF FASTENERS AT THE BS 1720 CIRCUMFERENTIAL BUTT SPLICE. THIS REPAIR HAS NO HISTORY IN AMIS & REQUIRES VALIDATION TO THE SRM. REMOVED EXISTINGDec 15, 2015 · N505UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201512133981Seat Track · damagedBS 988, BL 45.5, SEAT TRACK CROWN, SUPPORT INNER FLANGE FOUND ONE ELONGATED HOLE. REPAIRED IAW EA F-5310-T0321399 PART 1. REPAIR CLASSIFIED AS MAJOR.Dec 13, 2015 · N777FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201512123979Idg · failedRTO IMITATED ABOVE 40KTS IAS BUT LESS THAN 80 KTS IAS DUE TOTAL ELEC FAILURE, EXCEPT FOR BATTERY POWER, DURING THE TAKEOFF ROLL ON RWY 17L. PERFORMED BITE CHECK OF BPCU. NR 1, 9 LT & UNDER FREQ TRIP, IDG & PMG WIRING, IDG HIGH RISE TEMP, NR 2 RT BP TRIP, NRDec 12, 2015 · N775FD · Boeing 757222 · AC Generator-AlternatorSDR FDEA201512103969Skin · damagedMAIN DECK CARGO DOOR HAS PUNCTURE DAMAGE AT STRINGER 9, STATION 510 & A CREASE THAT EXTENDS FROM THE TOP OF THE PUNCTURE DAMAGE TO STRINGER 7. THERE IS ALSO A GOUGE JUST FWD OF THE PUNCTURE DAMAGE. REPAIRED MAIN DECK CARGO DOOR, BETWEEN STATION 500 & 520, BEDec 10, 2015 · N791FD · Boeing 757222 · Cargo/Baggage DoorsSDR FDEA201512103964Floorbeam · corrodedCABIN BS 1640, FLOORBEAM EXISTING REPAIR HAS CORROSION. COMPLIED WITH EA F-5310-T0321037 PART 1. REPAIR CLASSIFIED AS MAJOR.Dec 10, 2015 · N777FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201512103963Floorbeam · corrodedBS 1640, FLOORBEAM HAS CORROSION. REPAIRED IAW EA F-5310-T0321037 PART 1. REPAIR CLASSIFIED AS MAJOR.Dec 10, 2015 · N777FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201512083950Adapter · corrodedFUEL TANKS, LT WING TANK OVERWING FILL PORT ADAPTER MATING SURFACE CORRODED. REMOVED CORROSION FROM LT OVERWING FILL PORT ADAPTER MATING SURFACE IAW SRM 51-10-02, OUT OF LIMITS IAW SRM 57-20-01-1A STEP 3E. REPAIRED LT WING TANK FILL PORT ADAPTER MATING SURFADec 8, 2015 · N791FD · Boeing 757222 · Wing Miscellaneous StructureSDR FDEA201512083948Frame · corrodedAFT CARGO BAY FRAME, BS 1200 LBL 2.9 TO RBL 2.9, HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02. REWORK AREA FOUND OUT OF LIMITS IAW SRM 53-00-07-1 FIG 101 DETAIL II. R & R FRAME IAW SRM 51-40-02 & DWG 146N1028 CAT A REPAIR. MAJOR REPAIR.Dec 8, 2015 · N791FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201512073929Skin · chafedPANEL 655AR EXTERNAL SKIN HAS CHAFED. REPAIRED IAW EA F5750-T0320958. MAJOR REPAIR.Dec 7, 2015 · N788FD · Boeing 757222 · Wing, Plate/SkinSDR FDEA201512073938Adapter · corrodedFUEL TANKS, RT WING TANK OVERWING FILL PORT ADAPTER MATING SURFACE CORRODED. REMOVED CORROSION FROM RT OVERWING FILL PORT ADAPTER MATING SURFACE IAW SRM 51-0-02, OUT OF LIMITS IAW SRM 57-20-01-1A STEP 3E. REPAIRED RT WING OVERWING FILL PORT ADAPTER MATING SUDec 7, 2015 · N791FD · Boeing 757222 · Fuel StorageSDR FDEA201512073939Door Sill · corrodedAFT CARGO DOOR, LOWER SILL INBD CHORD, LOWER SURFACE UNDER & AROUND NUTPLATES, CORRODED. REMOVED CORROSION IAW SRM 51-10-02. NO ALLOWABLE DAMAGE NOTED IN SRM. R & R INBD UPPER CHORD FROM STATION 1360 - 1460, IAW SRM 51-40-02 & DWG 146N8522. MAJOR REPAIRDec 7, 2015 · N791FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201512033882Frame · corrodedAFT PIT FRAME STATION 1340, STRINGER 26R HAS CORROSION. REMOVED CORROSION IAW SRM-51-10-02, REWORK AREA, FOUND OUT OF LIMITS IAW SRM-53-00-07-1 FIG 101 DETAIL II. R & R FRAME AT STATION 1340 FROM STRINGER 24L - 24R IAW SRM-51-40-02 & DWG 146N1008 CAT A MAJORDec 3, 2015 · N791FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201512033881Skin · damagedINCOMING, LIGHTNING STRIKE BLEND OUT REPAIR THAT EXCEEDS THE SRM LIMITS AT BS 853, STRINGER 8L, 6TH & 7TH RIVETS FWD OF BS 860. REF UAL-IND-00-01028F. REPAIRED INCOMING BLENDED OUT AREA IAW-SRM-53-00-01 FIG 201 REPAIR 15 AT STATION 840- 860, BETWEEN STRINGEDec 3, 2015 · N791FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201512023856Liner · out of position1L ENTRY DOOR NOT ARMING PROPERLY. WHEN ARMED & DISARMED LEVER PLACED IN ARMED POSITION. THE KNUCKLE BUSTER INDICATOR STAYS IN FLUSH POSITION. PERFORMED FIM 52-11 FAULT TREE 813 ITEMS 1 - 6. REMOVED COVER & LOWER LINING INTERIOR HANDLE, ADJUSTED LOWER LINIDec 2, 2015 · N770FD · Boeing 757222 · Passenger/Crew DoorsSDR FDEA201511293814Skin Panel · chafedRIGHT WING, OTBD NOSE SKIN FOUND CHAFED AT 2.5" FROM OTBD EDGE. NOSE SKIN R & R IAW SRM 51-40-02 REV 116 & DWG 113N3500 SHT 3 REV D. REPAIR CLASSIFIED AS MAJOR.Nov 29, 2015 · N777FD · Boeing 757222 · Wing, Plate/SkinSDR FDEA201511253777Skin · dentedREWORK OF NR N00207, VERTICAL STAB LT SIDE AUXILIARY PANEL HAS DENT, 14" FROM AUXILIARY SPAR & 56" FROM BOTTOM, DUE TO PER NOTED SRM. A VISUAL & NDT INSPECTION OF DAMAGED AREA FOR DISBONDS, DELAMINATION, IS REQUIRED PRIOR TO APPLYING REPAIR. THIS WAS NOT DOCNov 25, 2015 · N788FD · Boeing 757222 · Vertical Stabilizer, Plate/Skin
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