Boeing 757-2S7

Service difficulty reports · 1,282

Newest first. General aviation reporting is voluntary.

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 = '7572S7'
  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 FDEA201105071777Stringer · misrepairedEXISTING STRINGER REPAIRS AT STA 1450-1470, STR 28L REQUIRES REPLACEMENT DUE TO NOT BEING INSTALLED IAW APPROVED DATA. REMOVED AND REPLACED EXISTING STRINGER REPAIRS, BS 1450-1479, S28L, PER SRM 53-00- 03, REPAIR NR 2, DETAIL 1. FABRICATED HAT SECTION, 2EA.,May 7, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Longeron/StringerSDR FDEA201105071776Skin · misrepairedFUSELAGE EXTERNAL SKIN REPAIR AT STA 540-550, STR-27L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH KNOWN APPROVED DATA. R & R DOUBLER & FILLER STA 540-550 STR -27L IAW SRM 51-40-02 /SRM 53-00-01, FIG 201, TABLE I - III, REPAIR 15, W/ DOUBLER PN 2024-T3-071May 7, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Plate/SkinSDR FDEA201105051759Skin · misrepairedEXISTING EXTERNAL FUSELAGE SKIN REPAIR AT STA. 740, STR 25R REQUIRES REPLACEMENT DUE TO NOT BEING IN COMPLIANCE WITH APPROVED DATA. REMOVED EXISTING DOUBLER/FILLER, BS 730-750, S-25R. HFEC INSP. SKIN CUTOUT, INITIAL HOLES PER NTM 51-00-19, PT.6 AND NTM 51-00May 5, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Plate/SkinSDR FDEA201105041751Skin · misrepairedSKIN REPAIR AT STA.740-760, STR 27R TO 28R REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH KNOWN APPROVED DATA. REMOVED DOUBLER/FILLER AT BS 740-760, S-27R-S-28R, PER SRM 51-40-02. HFEC SKIN CUTOUT, INITIAL HOLES PER NTM 51-00-19, PT.6, AND NTM 51-00-16, PT.6. May 4, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Plate/SkinSDR USAA20110429BB034Slide · low pressurePHX - THE L4 DOOR EVACUATION SLIDE PRESSURE GAUGE IS IN THE RED. MAINTENANCE REMOVED AND REPLACED THE L4 DOOR SLIDE.Apr 29, 2011 · N906AW · Boeing 7572S7 · Escape SlideSDR FDEA201104251618Channel · mismanufacturedUNABLE TO INSTALL CHANNEL SPLICE, BETWEEN STA 1620 TO STA 1640, RBL 60, WL 208.1, WILL HAVE SHORT EDGE CONDITION AT (1 EA) 0.100 HOLE LOCATION AT BS 1620 - 1640 RBL 60 A CREASE BEAM REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON MApr 25, 2011 · N926FD · Boeing 7572S7 · Fuselage Miscellaneous StructureSDR USAA2011041891508Switch · brokenMCN - C1 - L2 DOOR EMERGENCY LIGHTS TEST SWITCH BROKEN. REPLACED L2 DOOR EMERGENCY LIGHTS TEST SWITCH AS REQUIRED. OPS TEST GOOD IAW B757 AMM 31-51-00 TEMP REVISION 33-019AW.Apr 16, 2011 · N902AW · Boeing 7572S7 · Emergency LightingSDR USAA2011041391485Intercostal · corrodedMCN - C1 CHECK - CORROSION ON INTERCOSTAL AT BS 1505, S25L - S26L. REPLACED INTERCOSTAL AT BS 1505, S25L - S26L IAW B757 SRM 51-30-01.Apr 9, 2011 · N902AW · Boeing 7572S7 · Fuselage Miscellaneous StructureSDR FDEA201104061366Frame · gougedFRAME AT BS 1140, S2L, IS GOUGED. REMOVED DAMAGED SECTION OF FRAME IAW SRM 51-40-02. LOCATED, TRIMMED AND DRILLED FRAME AND SPLICES SRM 53-00-07, P.201/202, FIG 201. TREATED AND PRIMED FRAME AND SPLICES IAW SRM 51-20-01. INSTALLED FRAME REPLACEMENT AND 4 EApr 6, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, FrameSDR USAA2011041891512Strut · corrodedMCN - C1 - CORROSION ON RIGHT SIDE LOWER FORWARD AREA OF INNER BORE OF NOSE LANDING GEAR STRUT LOWER TORSION LINK LUG. REPLACED NOSE LANDING GEAR INNER CYLINDER ASSEMBLY LOWER STRUT IAW B757 32-51-11-4, 32-51-00-5 & 32-34-00-5.Mar 30, 2011 · N902AW · Boeing 7572S7 · Nose/Tail Landing Gear Strut/AxleSDR USAA2011041891511Strap · crackedMCN - C1 - CRACK ON FLOORBEAM STABILIZATION STRAP AT BS 1620, RBL 24.75. REPAIRED FLOORBEAM STABILIZATION STRAP AT BS 1620, RBL 24.75 IAW B757 SRM 51-70-13.Mar 30, 2011 · N902AW · Boeing 7572S7 · Fuselage Main, Floor BeamSDR USAA2011041891510Collar · corrodedMCN - C1 - CORROSION ON INNER BORE OF NOSE LANDING GEAR STEERING COLLAR UPPER TORSION LINK LUG. REPLACED NOSE LANDING GEAR STEERING COLLAR IAW B757 AMM 32-51-11-4, 32-51-00-5 & 32-34-00-5.Mar 30, 2011 · N902AW · Boeing 7572S7 · Landing Gear Steering SystemSDR USAA2011041191397Reveal · crackedMCN - C1 CHECK - CRACKED REVEAL STRIP ASSEMBLY ON THE AFT CARGO DOOR AT BS 1380, S26R. REPLACED REVEAL STRIP ASSEMBLY ON THE AFT CARGO DOOR AT BS 1380, S26R IAW B757-200 SRM 51-70-13, FIGURE 1.Mar 30, 2011 · N902AW · Boeing 7572S7 · Cargo/Baggage DoorsSDR FDEA201103291235Frame · damagedSECTION 46, STA 1640, LBL63.0 BETWEEN WL207-200 UNABLE TO LOCATE 657N3161-11 FITTING DUE TO EXISTING FASTENER HOLES ON THE FRAME, 2 EA ARE NOT POSITIONED AS DEPICTED ON DWG 657N3160, SH 2, REV D -FIGURE "E". AT BS 1640, LBL 63, WL 207, FRAME REPAIR WAS ACCOMMar 29, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, FrameSDR USAA2011041491494Intercostal · corrodedMCN - C1 CHECK - CORROSION ON INTERCOSTAL AT BS 1300 - BS 1320, LBL 17. REPLACED INTERCOSTAL AT BS 1300 - BS 1320, LBL 17 IAW B757 SRM 51-40-02.Mar 29, 2011 · N902AW · Boeing 7572S7 · Fuselage Miscellaneous StructureSDR USAA2011041491493Seat Track · crackedMCN - C1 CHECK - CRACKED SEAT TRACK SUPPORT BEAM AT BS 880, LBL 45.50. REPAIRED SEAT TRACK SUPPORT BEAM AT BS 880, LBL 45.50 IAW EA 130554.Mar 29, 2011 · N902AW · Boeing 7572S7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201103291234Seat Track · damagedSEAT TRACK INSTL SEC46 UNABLE TO INSTALL 657N3311-1 SPLICE FITTING AT STA 1280 LBL 45.50, EXISTING FASTENER HOLES ON FLOORBEAM WEB ARE NOT POSITIONED ON DWG 657N3311, SH 5 AND SEAT TRACK 657N3318-7 REQ TO TRIM FWD EDGE FLANGE .300 APPROX TO MAINTAIN .10Mar 29, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Floor BeamSDR USAA2011041891509Stop Fitting · corrodedMCN - C1 - CORROSION ON L1 DOOR STOP FITTING, NR 4 FROM THE TOP AT BS 377.7, S12L. REPLACED L1 DOOR STOP FITTING, NR 4 FROM THE TOP AT BS 377.7, S12L IAW B757 AMM 20-11-00-2.Mar 26, 2011 · N902AW · Boeing 7572S7 · Passenger/Crew DoorsSDR FDEA201103231284Beam · crackedVERTICAL STABILIZER LT FIXED T/E BEAM IS CRACKED AT RUD STA 97.354 SDR ENTERED IN ERROR. CONSIDERED MINOR REPAIRMar 23, 2011 · N926FD · Boeing 7572S7 · Vertical StabilizerSDR FDEA201103231680Skin · misrepairedEXISTING FUSELAGE SKIN REPAIR AT STA 274-285, STR 16L REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH KNOWN APPROVED DATA. REMOVED AND REPLACED EXTERNAL FUSELAGE SKIN DOUBLER / REPAIR AT STA 274- 285, STR 16L IAW SRM 53-00-01 FIG 201 REPAIR 15. CAT. "B" REMar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Plate/SkinSDR FDEA201103231587Crease Beam · damagedUNABLE TO INSTALL 657N4308-1 CHANNEL SPLICE, BETWEEN STA.1620 TO STA 1640, LBL60.00 WL208.1; WILL HAVE SHORT EDGE MARGIN CONDITION AT -1 EA.- 0.10" HOLE LOCATION. AT BS 1640, LBL60, WL208 A CREASE BEAM REPAIR WAS ACCOMPLISHED. CLASSIFIED AS A MAJOR.Mar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, StructureSDR FDEA201103231521Sill · misrepairedREPAIR ON DOOR SILL/CREASE BEAM AT STA 1370, WL 208, RBL 62 REQUIRES REPLACEMENT DUE TO NOT COMPLYING WITH APPROVED DATA. R & R CREASE BEAM CHORD, FROM BS 1290-1405, RBL 62, PN: 146N8326-2, BATCH NR 2032339, IAW SRM 51-40-02, AND DWG 146N8326. MAJOR REPAIRMar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage Miscellaneous StructureSDR FDEA201103231504Frame · damagedFRAME STA 1640, RBL 63, WL 208 HAS INCOMING DAMAGE, 2 EA AREAS ON INBD J ANGLE, 2 EA GOUGES AND THE WEB HAS CUT. FRAME REPAIREDMar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, FrameSDR FDEA201103231283Frame · gougedFRAME STA 1640, RBL63, WL208 HAS 2 EA AREAS OF DAMAGE INBD JANGLE HAS EEA GOUGES AND THE AFT FRAME WEB HAS CUT (INCOMING DAMAGE FOUND AFTER FLOORBEAM REMOVAL) THIS SDR WAS GENERATED IN ERROR. THE ABOVE DISCREPANCY IS CAPTURED ON THE FAA FORM 337, WHICH IS ISSUMar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, FrameSDR FDEA201103231408Skin · misrepairedFUSELAGE SKIN REPAIR 60" AFT OF L2 DOOR, 6" ABOVE FLOORLINE REQUIRES REPLACEMENT, DUE TO NOT COMPLYING TO APPROVED DATA. REMOVED AND REPLACED DOUBLER AT BS 775, S16L-S17L, PER SRM 51-40-02, AND SRM 53-00- 01, REPAIR 16, BATCH 1928869, PER SRM 53-00-01, FIG.2Mar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Plate/SkinSDR FDEA201103231186Seat Track · gougedSEAT TRACK AT STA 1075-1180, RBL45.50 HAS SEVERAL NICKS, GOUGES AND DAMAGED DOME NUTS. SEAT TRACK FROM BS 1075-1180, RBL 45.5, OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1, P 102. FABRICATED NEW SEAT TRACK, PN BAC 1520-792, BATCH NR 00019046632 AND INMar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201103231185Seat Track · gougedSEAT TRACK AT RBL24.75 FROM STA 1075-1180 HAS SEVERAL NICKS, GOUGES AND DAMAGED DOME NUTS, SEAT TRACK FROM BS 1075-1180, RBL 24.75 OUT OF LIMITS IAW SRM 53-00-52, FIG101, DETAIL 1, P.102. FABRICATED NEW SEAT TRACK, PN BAC 1520-792, BATCH NR 000194663 AND INSMar 23, 2011 · N926FD · Boeing 7572S7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201103181077Beam · misinstalledUNABLE TO INSTALL 657N3338-36 SPLICE AND 657N338-30 ANGLE CLIP AT STA 1180 RT DUE TO THE INCOMING CONDITION OF THE 144N5214-1 RT INBD CHORD LOCATION TOO FAR INBD. REPAIR WAS ACCOMPLISHED, DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION , ON MAE MOD W/C 11Mar 18, 2011 · N926FD · Boeing 7572S7 · Fuselage Miscellaneous StructureSDR USAA2011032191155Pin · backed outMCN - C1 - EEL - LOWER LEFT EMERGENCY LIGHT NEXT TO L-3 DOOR SAYING "EXIT" IS INOP. RESEATED PUSHED BACK PIN ON LOWER LEFT EMERGENCY LIGHT NEXT TO L-3 DOOR SAYING "EXIT" AS REQUIRED. OPS CHECK GOOD.Mar 13, 2011 · N905AW · Boeing 7572S7 · Light System WiringSDR USAA20110315BB018Transmission · lack of lubeLIH FLT 146 EN ROUTE PHX TO LIH. ON FINAL APPROACH, AFTER SELECTING FLAPS 25, THE CREW RECEIVED AN EICAS MESSAGE OF T/E FLAP DISAGREE. THE CREW PERFORMED A GO-AROUND AND COMPLETED THE APPROPRIATE QRH PROCEDURES. ON NEW APPROACH, THE CREW SELECTED FLAPS 20Mar 13, 2011 · N902AW · Boeing 7572S7 · Trailing Edge Flap Control SystemSDR USAA2011031691064Battery · weakMCN - C1 - EEL - L-2 DOOR FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY IS WEAK. REPLACED L-2 DOOR FLIGHT ATTENDANT EMERGENCY FLASHLIGHT BATTERY AS NEEDED. OPS CHECK GOOD.Mar 11, 2011 · N905AW · Boeing 7572S7 · Emergency EquipmentSDR FDEA201103100930Floor Support · corrodedAFT CARGO STA. 1400 TO STA.1420 AT BL 0 FLOOR SUPPORT WEB HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-00-53, FIG. 101 DETAIL V, REMOVED AND REPLACED FLOOR SUPPORT WEB IAW SRM 51-40- 02 AND SRM 53-00-53, REPAIR CLASSIFIMar 10, 2011 · N926FD · Boeing 7572S7 · Fuselage Miscellaneous StructureSDR USAA2011031591061Fitting · crackedMCN - C1 - MAJOR REPAIR - CRACK ON CLIP AT BS 865, BL 0. REPLACED CLIP AT BS 865, BL 0 IAW B757 SRM 51-40-02.Mar 5, 2011 · N905AW · Boeing 7572S7 · Fuselage Miscellaneous StructureSDR FDEA201103030833Floorbeam · misalignedSTA 700 INCOMING REPAIR AT RBL40 WILL INTERFERE WITH PTF MOD. R & R FLOORBEAM AT STA 700, BETWEEN RBL 70 TO LBL 70". BAC1518-338/18A, BATCH NR 0001922129, IAW SRM 53-30-51, FIG 1, PAG-4 AND SRM 51-40-02, AND REINSTALLED ATTACH PARTS, FROM ITEM 3 THRU 12, IAWMar 3, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Floor BeamSDR USAA20110303BB014Wire · damagedLIH - FLT 146 EN ROUTE PHX TO LIH. THE LEFT ENGINE HAD AN INTERMITTENT ENGINE FIRE INDICATION. MAINTENANCE ACCOMPLISHED A TEMPORARY WIRE REPAIR AT THE SIX O'CLOCK, INBOARD SIDE, AFT OF GEAR BOX.Mar 2, 2011 · N902AW · Boeing 7572S7 · Fire Protection System WiringSDR USAA2011030991008Panel · crackedMCN - C1 - MAJOR REPAIR - CRACK ON LEFT WING NR 2 SLAT COVE PANEL AT WS 580. REPLACED LEFT WING NR 2 SLAT COVE PANEL AT WS 580 IAW B757 SRM 51-40-02.Feb 24, 2011 · N905AW · Boeing 7572S7 · Leading Edge DevicesSDR FDEA201102220679Floorbeam · corrodedSTA 377, FLOORBEAM, LBL-60 HAS CORROSION ON LAWER SIDE OF UPPER FLANGE AROUND NUT PLATE HOLES. REMOVED CORROSION AND CHECK LIMITS ORIG MAT. 0.125 AFTER REWORK 0.050. FOUND OUT OF LIMITS IAW SRM 53-00-51 DET III. R & R FLOORBEAM IAW SRM 51-40-02 WITH MAT PFeb 22, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Floor BeamSDR FDEA201102190631Frame · gougedFRAME AT STA 1280 HAS GOUGES BETWEEN AREAS OF STR 11R-17R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL 2, P103; ORIGINAL MATERIAL IS .071", AFTER REWORK IS .050", LOSS IS .021". R & R FRAME SPLICE AT BS 1282, S12R-S13R, IAW SRM 53-00-07, FIG Feb 19, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, FrameSDR FDEA201102170595Seat Track · gougedBS 418-440, RBL 24, SEAT TRACK GOUGED. BLENDED AREA IAW SRM 53-00-52, FIG 101, DETAIL 1. CHECKED LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1, AND FOUND OUT OF LIMITS; BEFORE: .53", AFTER: .47", LOSS: .060". REMOVED SEAT TRACK IAW SRM 51-40-02, AT BS 418-440, RFeb 17, 2011 · N926FD · Boeing 7572S7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102170594Seat Track · gougedBS 418-440, RBL 45, SEAT TRACK GOUGED. BLENDED AREA AND CHECKED LIMITS IAW SRM 53-00-52. ORIGINAL MATERIAL WAS .053", AFTER REWORKIS .047", LOSS WAS .060", FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 1. REMOVED SEAT TRACK AT BS 418-440, RBL 45, IAWFeb 17, 2011 · N926FD · Boeing 7572S7 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201102120549Frame · gougedMDC FRAME AT STA 1280 HAS GOUGES ON AREAS BETWEEN STR S11L & S17L. REPAIRED IAW EA F-5310-146523, MAJOR REPAIR.Feb 12, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, FrameSDR FDEA201102110535Floorbeam · corrodedMAIN DECK, BS 365.25 FLOORBEAM, BETWEEN RBL 45 - 58, UNDERNEATH UPPER CHORD, HAS CORROSION AROUND NUT PLATE HOLES. REMOVED CORROSION BY BLENDING AREA IAW SRM 51-10-02 AREA OUT OF LIMITS. ORIGINAL MAT .125 AFTER REWORK .077 EXCEEDS MAX ALLOWABLE DAMAGE OF 10 PFeb 11, 2011 · N926FD · Boeing 7572S7 · Fuselage Main, Floor BeamSDR USAA2011020190482Wire · brokenMCN - C1 - EEL - CABIN BULLNOSE EMERGENCY LIGHT ABOVE SEAT ROW 15R DOES NOT ILLUMINATE WHEN TESTED. REPAIRED BROKEN WIRE WITH NEW TERMINAL IAW B757 SWPM 20-30-11 AT SEAT ROW 15R, OPS CHECK GOOD IAW B757 AMM 33-51-05-2.Jan 28, 2011 · N901AW · Boeing 7572S7 · Light System WiringSDR USAA2011013190407Switch · failedMCN - C1 - EEL - L-2 DOOR EMERGENCY LIGHT TEST SWITCH DOES NOT ILLUMINATE EMERGENCY LIGHTS. REPLACED L-2 DOOR EMERGENCY LIGHT TEST SWITCH IAW B757 AMM 33-51-05-02.Jan 28, 2011 · N901AW · Boeing 7572S7 · Emergency LightingSDR USAA2011012090304Attach Angle · crackedMCN - C1 - MAJOR REPAIR - CRACK ON INTERCOSTAL ATTACH ANGLE BETWEEN BS 440 TO BS 460, BL 0. REPLACED INTERCOSTAL ATTACH ANGLE BETWEEN BS 440 TO BS 460, BL 0 IAW B757 SRM 51-40-02.Jan 12, 2011 · N901AW · Boeing 7572S7 · Fuselage Miscellaneous StructureSDR USAA2011012090303Attach Angle · crackedMCN - C1 - MAJOR REPAIR - CRACK ON INTERCOSTAL ATTACH ANGLE BETWEEN BS 480 TO BS 500, RBL 9. REPLACED INTERCOSTAL ATTACH ANGLE BETWEEN BS 480 TO BS 500, RBL 9 IAW B757 SRM 51-40-02.Jan 12, 2011 · N901AW · Boeing 7572S7 · Fuselage Miscellaneous StructureSDR USAA2011012090305Stringer · corrodedMCN - C1 - MAJOR REPAIR - CORROSION ON STRINGER AT BS 1620, S28L. REPAIRED STRINGER AT BS 1620, S28L IAW B757 SRM 53-00-03.Jan 9, 2011 · N901AW · Boeing 7572S7 · Fuselage Main, Longeron/StringerSDR USAA20110111BB002Spring · bentPHX - THE L4 DOOR GIRT BAR SPRING WAS BENT. MAINTENANCE REPLACED THE L4 DOOR GIRT BAR.Jan 8, 2011 · N906AW · Boeing 7572S7 · Emergency EquipmentSDR USAA20101210BB088Slide · low pressurePHX - THE DOOR SLIDE AT DOOR L2 INDICATES BELOW THE GREEN BAND. MAINTENANCE REMOVED AND REPLACED THE L2 DOOR SLIDE.Dec 10, 2010 · N906AW · Boeing 7572S7 · Escape SlideSDR USAA20101126BB079Girt Bar · defectivePHX - THE GIRT BAR ENGAGEMENT LIGHT EXTINGUISHED WITH THE EVACUATION SLIDE ARMING LEVER IN ENGAGE POSITION AT SERVICE DOOR R1. REMOVED AND REPLACED THE R1 GIRT BAR ASSEMBLY.Nov 24, 2010 · N906AW · Boeing 7572S7 · Emergency Equipment
Back to Boeing 757-2S7