Boeing 737-900ER

Service difficulty reports · 1,008

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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 = '737900ER'
  ORDER BY difficulty_date DESC"

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SDR ASAA2024021248119Web · corrodedAFT CARGO THRESHOLD SILL HAS CORROSION. GROUNDED - YES. EVALUATED DAMAGE AND REMOVED CORROSION IAW B737-900ER SRM 53-00-53-1A-2 ORIGINAL MAT'L THKS .045 PER B737-900ER SRM 53-60-53-01-2 TABLE 2 REMOVED .022 MAT AND HAD .023 MAT'L, FOUND TO BE OUT OF LIMITS IAWFeb 12, 2024 · N403AS · Boeing 737900ER · Fuselage Miscellaneous StructureSDR DALA2024012501117Mechanism · misinstalled(LOG 5002778) IN REF WITH W/C 5200-01077-01B FOUND RH FWD LOWER SPRING MECHANISM HARDWARE MISSING. INSTALLED ALL REQUIRED HARDWARE PER B737 AMM 52-23-02.Jan 22, 2024 · N903DN · Boeing 737900ER · Emergency ExitsSDR DALA2024012501115Bolt · misinstalled(LOG 0166296) WHOLE PERFORMING W/C #5200-01077-01B FOUND BOTH RH VERTICAL MOVEMENT ARRESTOR BOLTS INSTALLED BACKWARDS. REINSTALLED HARDWARE (2EA.) IN CORRECT ORIENTATION ON BOTH RH VERTICAL MOVEMENT ARRESTORS REF B737 AMM 52-23.Jan 22, 2024 · N910DU · Boeing 737900ER · Emergency ExitsSDR DALA2024012501114Bolt · misinstalled(LOG 0166290) WHILE PERFORMING W/C #5200-01077-01A FOUND BOTH LH VERTICAL MOVEMENT ARRESTOR BOLTS INSTALLED BACKWARDS. INSTALLED HARDWARE (2EA.) ON BOTH LH VERTICAL MOVEMENT ARRESTORS IN CORRECT ORIENTATION REF. B737 AMM 52-23.Jan 22, 2024 · N910DU · Boeing 737900ER · Emergency ExitsSDR DALA2024012501113Nut · loose(LOG 5604122) DURING WORK CARD 5200-01077-01B FOUND RH FWD UPPER GUIDE NUT LOOSE. TORQUED RH FWD UPPER GUIDE BOLT NUT PER B737 AMM 52-23-02. COTTER PIN INSTALLED. OK FOR SVC.Jan 22, 2024 · N886DN · Boeing 737900ER · Emergency ExitsSDR DALA2024012501112Mechanism · wrong part(LOG 5385875) DURING INSPECTION OF RH MID EXIT DOOR PLUG. FOUND INCORRECT HARDWARE ON FWD LOWER SPRING MECHANISM. INSTALLED CORRECT HARDWARE AT RH PLUG FWD LOWER SPRING MECHANISM PER B737 AMM 52-23 AND REINSTALLED SIDEWALL PANEL PER B737 AMM 25-21.Jan 22, 2024 · N872DN · Boeing 737900ER · Emergency ExitsSDR CALA2024012400222Connector · unknownLOW SPEED REJECT FOR AIR CONDITIONING UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC METER INITIATED FOR WITH VENDOR ID V939095 MAC RELATED WORK ORDER 000000003095479 AND PRTR ANTI-ICE AND MASTER CAUTION ILLUMIJan 22, 2024 · N69835 · Boeing 737900ER · Ice/Rain Protection System WiringSDR DALA2024012301042Cabin Pressure · unknownSHIP 3895 - PRESS / DE - DUE TO CABIN ALTITUDE WARNING. FLIGHT DESCENDED TO 18,000 FEET AND CONTINUED. CORRECTIVE ACTION: PERFORMED DCPC 1-2 BITE CHECKS. NO TROUBLE FOUND. REPLACED BOTH CABIN PRESSURE ALTITUDE SWITCHES S128 AND S1153. PERFORMED SINGLE PACK CONJan 22, 2024 · N895DN · Boeing 737900ER · Cabin Pressure Control SystemSDR DALA2024012301040Nut · loose(LOG 5604123) DURING WORK CARD 5200-01077-01B. FOUND AFT RH UPPER GUIDE NUT LOOSE. TORQUED RH AFT UPPER GUIDE BOLT NUT PER B737 AMM 52-23-02. COTTER PIN INSTALLED. OK FOR SVC.Jan 22, 2024 · N886DN · Boeing 737900ER · Emergency ExitsSDR CALA2024012400221Cover · missingON ARRIVAL FOUND LH LOWER MOST OUTBD HORIZ STAB TO ELEV HINGE COVER MISSING. ON WALKAROUND, FOUND LH LOWER HORIZONTAL STAB TO ELEVATOR HINGE PANEL 334NB (MOST OTBD) MISSING., PNL 334NB, PN 185A1621-119, NIS SAN. PICS ADDED CORRECTION FOR ABOVE PN - SHOULD STAJan 19, 2024 · N62895 · Boeing 737900ER · Elevator StructureSDR DALA2024012301043Battery Pack · inoperative(LOG 5055163) SEAT MOUNTED EMERGANCY LIGHTS AT ROW 22-27 INOP. REPLACED BATTERY PACK FOR SEAT ROW 22 TO 27 PER B737-AMM-33-51-06. LIGHTS OPS NML.Jan 19, 2024 · N867DN · Boeing 737900ER · Emergency LightingSDR DALA2024012200933Skin · gouged(LOG 0160521) GOUGE IN FUSELAGE SKIN ABOVE R/H HORIZONTAL STAB BELOW STRINGER 4R BETWEEN STA 1121 & 1138. C/W ER/A 615068-14 REV ORIGINAL.Jan 18, 2024 · N895DN · Boeing 737900ER · Fuselage Main, Plate/SkinSDR ASAA2024011647461Baffle · corrodedAFT PIT RIGHT SIDE STIFFENER HAS CORROSION ATTACH WITH TRANSITION PANEL AT BS747 AND BS767 STR25R AND STR26R AS MARK STREAMER ATTACH. GROUNDED - YES. REMOVED CORROSION AT STA BS747 AND STA BS767 STR 25R AND STR 26R, ORIGINAL MAT .032, MAT REMOVED .007, REMAINIJan 16, 2024 · N292AK · Boeing 737900ER · Fuselage Main, Plate/SkinSDR ASAA2024012417460Intercostal · corrodedAFT PIT RIGHT SIDE TRANSITION PANEL HAS UPPER AND LOWER SURFACE HAS CORROSION NUMEROUS PLACE BETWEEN BS727I+10 AND BD727 STR26R AS MARK GROUNDED - YES. REMOVED CORROSION ORIGINAL THICKNESS .040, REMOVED .006, REMAINING THICKNESS .034 FOUND TO BE OUT OF LIMITS Jan 16, 2024 · N292AK · Boeing 737900ER · Fuselage Main, Plate/SkinSDR DALA2024011600601Skin · gouged(LOG 4412634) GOUGE ON SKIN AT APPROX 2" AFT OF STA 727F BETWEEN STRINGER 21L AND 22L. DOUBLERS DRILLED UP AND FABRICATED PER SRM 53-00-01-2R-36. TREATED AND PRIMED PARTS. INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01-2R-36.Jan 13, 2024 · N911DQ · Boeing 737900ER · Fuselage Main, Plate/SkinSDR ASAA2024011147286Slide · low pressureL2 DOOR NOT IN GREEN RANGE. GROUNDED - YES. VERIFIED L2 DOOR SLIDE PRESSURE LOW.REMOVED L2 DOOR SLIDE REF AMM 25-66-01-000-801. S. MICHAEL 19379 1/11/2024INSTALLED L2 DOOR SLIDE ( SERVICABLE SLIDE) MM 25-66-01.Jan 11, 2024 · N274AK · Boeing 737900ER · Escape SlideSDR ASAA2024011147282Floor Panel · corrodedFLOOR PANEL 147A5810-477 HAS CORRODED INSERTS. GROUNDED - YES. COMPLETED REMOVE AND REPLACE CORRODED INSERTS ON FLOOR PANEL 147A5810-477 IAW B737-900ER SRM 53-00-50-2R-0.Jan 11, 2024 · N292AK · Boeing 737900ER · Fuselage Floor PanelSDR ASAA2024011147281Floor Panel · damagedFLOOR PANEL 147A5810-573 HAS DAMAGED INSERTS. GROUNDED - YES. COMPLETED REMOVED AND REPLACE DAMAGED INSERTS ON FLOOR PANEL 147A 5810-573 IAW B737-900ER SRM 53-00-50-2R-0.Jan 11, 2024 · N292AK · Boeing 737900ER · Fuselage Floor PanelSDR ASAA2024011047459Floor Panel · delaminatedFLOOR PANEL #221BF HAS SURFACE DELAMINATION. GROUNDED - YES. REPAIRED FLOOR PANEL #221BF PN: 141A5810-729 IAW B737-900 SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0.Jan 10, 2024 · N292AK · Boeing 737900ER · Fuselage Floor PanelSDR ASAA2024011047280Floor Panel · damagedFLOOR PANEL 222DF HAS DAMAGED INSERT. GROUNDED - YES. COMPLETED REMOVE AND REPLACE INSERTS ON FLOOR PANEL #222DF IAW B737-900ER 53-00-50-2R-0.Jan 10, 2024 · N292AK · Boeing 737900ER · Fuselage Floor PanelSDR ASAA2024011047279Floor Panel · damagedFLOOR PANEL #221CF HAS DAMAGED INSERT. GROUNDED - YES. REMOVED AND REPLACED DAMAGED INSERT ON FLOOR PANEL 221CF IAW B737-900ER SRM 53-00-50-2R-0.Jan 10, 2024 · N292AK · Boeing 737900ER · Fuselage Floor PanelSDR DALA2024010800228Windshield · crackedSHIP 3887 -DIV- TO ATL DUE TO FIRST OFFICER'S R1 WINDSHIELD CRACKED. CORRECTIVE ACTION: REPLACED R1 WINDSHIELD AND HEAT CONTROLLER. OPS CHECKS GOOD.Jan 6, 2024 · N887DN · Boeing 737900ER · Flight Compartment WindowsSDR DALA2024010800225Unknown · unknown(LOG 5055116) ON WAKEUP FOUND EXPOSED BROKEN EMERGENCY PATH LIGHT WIRES AT SEAT 30 FED. REPAIRED BROKEN WIRES WITH SPLICE CONNECTOR & RE SECURED UNDER TRACK PROTECTOR. REF. B737 SWPM 20-10-13. EMERGENCY PATH LIGHTS OPS CK'S GOOD.Jan 4, 2024 · N867DN · Boeing 737900ER · Emergency LightingSDR DALA2024010800224Oven · damaged(LOG 4303384) F/A NOTICED A BURNING RUBBER ODOR IN FWD GALLEY. THE OVEN WAS TURNED OFF AND THE ODOR DISSIPATED. FOUND FOOD ITEMS IN CONTAINERS AND ONE ITEM COVERED IN PLASTIC. R/R FWD GALLEY OVEN PER B737 AMM 25-31-88. OVEN OPERATES NORMAL.Jan 4, 2024 · N913DU · Boeing 737900ER · Buffet/GalleysSDR ASAA2023123047372Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-443 DELAMINATED. GROUNDED - YES. ACCOMPLISHED PERMANENT CLASS A REPAIR OF DELAMINATION ON MAIN CABIN FLOOR PANEL 147A5810-443 IAW ASA B737-900ER SRM 53-00-50-2R-0 REPAIR 7, AND FIG 210.Dec 30, 2023 · N407AS · Boeing 737900ER · Fuselage Floor PanelSDR CALA2024010400020Fitting · gouged(B737-52-3-0690) L2 DOOR UPPER FORWARD DOOR STOP FITTING IS GOUGED. REMOVED GOUGED DOOR STOP FITTING AND INSTALLED NEW 147A6128U53 S TOP FITTING ASSY IAW BAC DWG 147A6116 REV B, 147A6128 REV D AND B737-900 SRM 51-40-02.Dec 29, 2023 · N68453 · Boeing 737900ER · Passenger/Crew DoorsSDR ASAA2024011747354Floor Panel · delaminatedFLOOR PANEL P/N 141A5810-155 DELAMINATED. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 141A5810-155 IAW B737-900 SRM 53-00-50-1A-1 AND SRM 53-00-50-2R-0.Dec 28, 2023 · N407AS · Boeing 737900ER · Fuselage Floor PanelSDR ASAA2024011747353Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-444. GROUNDED - YES. REPAIRED PANEL 147A5810-444 WITH CATEGORY A PERMANENT REPAIR IAW B737-900 SRM 53-00-50-1A-1, SRM 53-00-50-2R-0, SRM 53-00-50-2R-7.Dec 28, 2023 · N407AS · Boeing 737900ER · Fuselage Floor PanelSDR ASAA2023122847227Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-421 DELAMINATED. GROUNDED - YES. COMPLETED WET LAY UP REPAIR ON FLOOR PANEL P/N 147A5810-421 IAW B737-900ER SRM 53-00-50-2R.Dec 28, 2023 · N407AS · Boeing 737900ER · Fuselage Floor PanelSDR ASAA2023122747373Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-398 DELAMINATED. GROUNDED - YES. REPAIRED DELAMINATIONS ON PANEL PN: 147A5810-398 IAW B737-900ER SRM 53-00-50-2R-7.Dec 27, 2023 · N407AS · Boeing 737900ER · Fuselage Floor PanelSDR ASAA2024011747352Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-109 DELAMINATED. GROUNDED - YES. ACCOMPLISHED PERMANENT CLASS A REPAIR OF DELAMINATED FACE SHEET ON MAIN CABIN FLOOR PANEL 147A5810-109 IAW ASA B737-900ER SRM 53-00-50-2R-0, REPAIR 7, AND FIG 210.Dec 27, 2023 · N407AS · Boeing 737900ER · Fuselage Floor PanelSDR ASAA2024011747351Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-439 DELAMINATED. GROUNDED - YES. REPAIRED FLOOR PANEL P/N 147A5810-439 IAW B737-900 SRM 53-00-51-1A-1 AND SRM 53-00-50-2R-0.Dec 27, 2023 · N407AS · Boeing 737900ER · Fuselage Floor PanelSDR ASAA202011747350Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-398 DELAMINATED. GROUNDED - YES. REPAIRED DELAMINATIONS ON PANEL PN: 147A5810-398 IAW B737-900ER SRM 53-00-50-2R-7.Dec 27, 2023 · N407AS · Boeing 737900ER · Fuselage Floor PanelSDR ASAA2023122747040Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-446 DELAMINATED. GROUNDED - YES. EVALUATED AND REPAIRED FLOOR PANEL 147A5810-446 DELAM AND 1 INSERT IAW B737-900ER SRM 53-00-50-1A-1, SRM 53-00-50-2R-0, SRM 53-00-50-2R-7.Dec 27, 2023 · N407AS · Boeing 737900ER · Fuselage Floor PanelSDR ASAA2023122747039Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-445 DELAMINATED. GROUNDED - YES. REPAIRED DELAMINATION ON FLOOR PANEL PN 147A5810-445 IAW B737-900ER SRM 53-00-50-2R-7.Dec 27, 2023 · N407AS · Boeing 737900ER · Fuselage Floor PanelSDR ASAA2023122747038Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-440 DELAMINATED. GROUNDED - YES. EVALUATED FLOOR PANEL P/N 147A5810-440 AND FOUND MULTIPLE MISSING/PEELING UPPER SURFACE AND 4EA DAMAGED INSERTS REQUIRING REPAIR IAW ASA B737-900ER SRM 53-00-50-1A-1. REPAIRED IAW ASA B737-900ER SRM 53-Dec 27, 2023 · N407AS · Boeing 737900ER · Fuselage Floor PanelSDR ASAA2023122747037Floor Panel · delaminatedFLOOR PANEL P/N 147A5810-477 DELAMINATED. GROUNDED - YES. COMPLETED WET BY UP AND REMOVED AND REPLACED INSERTS 6EA ON FLOOR PANEL P/N 147A5810-477 IAW B737-900ER SRM 53-00-50-2R-0.Dec 27, 2023 · N407AS · Boeing 737900ER · Fuselage Floor PanelSDR CALA2023122803741Unknown · unknownFLP DISAGREE W HANDLE PERFORMED FLAP POSITION INDICATOR NEEDLES STICK PROBLEM FAULT. UNABLE TO DUPLICATE ISOLATION 27-51 TASK 842 NO FAULTS. NEEDLE MOVES SMOOTHLY THRU POSITIONS, FIM INDICATES INTERMITTENT FAULT. NO CURRENT FAULTS, NO FAULT HISTORY.Dec 26, 2023 · N39416 · Boeing 737900ER · Trailing Edge Flap Control SystemSDR ASAA2023122347374Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727I+9 TO 727L+13 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL STA 727I+9 TO 727L+13 IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIG. THICKNESS .040 IAW B737-900ER SRM 53-60-53-OI-2. 100% MAT LOSS &Dec 23, 2023 · N407AS · Boeing 737900ER · Fuselage Miscellaneous StructureSDR ASAA2024011747357Transition Panel · corrodedAFT PIT R/H TRANSITION PANEL STA 727 TO 727E+12 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM R/H TRANSITION AT STA 727-727E+12 IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIG THICKNESS .040 IAW B737-900ER SRM 53-60-53-OI-2 TABLE 2 100% MAT LOSS AND FOUND TO BEDec 23, 2023 · N407AS · Boeing 737900ER · Fuselage Miscellaneous StructureSDR ASAA2024011747356Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727 TO 727D+15 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL STA 727 TO 727D=15 IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIGINAL THICKNESS .040 IAW B737-900ER SRM 53-60-53-OI-2. 100% MAT LOSS & FODec 23, 2023 · N407AS · Boeing 737900ER · Fuselage Miscellaneous StructureSDR ASAA2024011747355Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727D+15 TO 727I+9 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL STA 727D+15 TO 727I+9 IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIG THICKNESS .040 IAW B737-900ER SRM 53-60-53-OI-2. 100% MAT LOSS & Dec 23, 2023 · N407AS · Boeing 737900ER · Fuselage Miscellaneous StructureSDR ASAA2024011747340Transition Panel · corrodedAFT PIT R/H TRANSITION PANEL STA 727E+12 TO727I+9 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM R/H TRANSITION AT STA 727E TO 727I IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIG THICKNESS " .040 IAW B737-900ER SRM 53-60-53-OI-7 TBALE 2 100% MAT LOSS AND FOUND Dec 23, 2023 · N407AS · Boeing 737900ER · Fuselage Miscellaneous StructureSDR ASAA2024011747339Transition Panel · corrodedAFT PIT L/H TRANSITION PANEL STA 727L+13 TO 809 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM AFT PIT L/H TRANSITION PANEL STA 727L+13 TO 809 IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIGINAL THICKNESS 0.04 IAW B737-900ER SRM 53-00-53-OI-2 100% MAT LOSS & FOUDec 23, 2023 · N407AS · Boeing 737900ER · Fuselage Miscellaneous StructureSDR ASAA2024011747338Transition Panel · corrodedAFT PIT R/H TRANSITION PANEL STA 727I+9 TO 767 HAS CORROSION. GROUNDED - YES. REMOVED DAMAGE FROM R/H TRANSITION AT STA 727+9-767 IAW B737-900ER SRM 2 53-00-53-1A-2.2.D ORIG THICKNESS .040 IAW B737-900ER SRM 53-60-53-OI-2 3 TABLE 2 100% MAT LOSS & FOUND TO BE Dec 23, 2023 · N407AS · Boeing 737900ER · Fuselage Miscellaneous StructureSDR ASAA2024011747337Angle · corrodedAFT PIT DOOR SURROUND, FWD SHELD ATTACH ANGLE HAS CORROSION. GROUNDED - YES. EVAULATED THE SHEILD ATTACH ANGLE CORROSION NO ALLOWABLE DAMG LIMITS GIVEN IN B737-900ER SRM REMOVED AND REPLACED NEW PART IAW B737-900ER SRM 51-40-02 AND BOEING DWG #146A8123.Dec 23, 2023 · N407AS · Boeing 737900ER · Fuselage Miscellaneous StructureSDR ASAA2023122347336Shield · corrodedAFT PIT DOOR SURROUND, FWD SHEILD HAS CORROSION. GROUNDED - YES. EVAULATED REMOVED CORROSION FROM SHEILD PER B737-900ER SRM 53-00-53-1H-2A ORIG THICKNESS IS .050 PER B737-900ER SRM 53-30-15-OI TABLE 4 REMOVED .007 REMAINING IS .043 AND FOUND TO BE OUT OF LIMITDec 23, 2023 · N407AS · Boeing 737900ER · Fuselage Miscellaneous StructureSDR ASAA2023122347335Transition Panel · corrodedFWD PIT L/H TRANSITION PANEL STA 500K+6 TO 500L HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT L/H TRANSITION PANEL AT STA 500K+6 TO 500L IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIG THICKNESS IS .040 IAW B737-900ER SRM 53-30-53-01-2 TABLE 2. RDec 23, 2023 · N407AS · Boeing 737900ER · Fuselage Miscellaneous StructureSDR ASAA2023122347334Transition Panel · corrodedFWD PIT R/H PANEL STA 500E+2 TO 500H+10 HAS CORROSION. GROUNDED - YES. REMOVED THE CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500E+2 TO 500HD+10 IAW B737-900ER SRM 53-00-53-1A-2.2.D. ORIG THICKNESS IS .040" IAW B737-900ER SRM 53-30-53-0I-2 TABLE 2.Dec 23, 2023 · N407AS · Boeing 737900ER · Fuselage Miscellaneous StructureSDR ASAA2023122347333Transition Panel · corrodedFWD PIT R/H TRANSITION PANEL STA 500H+10 TO 500L HAS CORROSION. GROUNDED - YES. REMOVED CORROSION FROM THE FWD PIT R/H TRANSITION PANEL AT STA 500H+10 TO 500L IAW B737-900ER SRM 53-00-53-1A-2.2.D ORIG THICKNESS IS .040" IAW B737-900ER SRM 53-30-53-01-2 TABLE 2Dec 23, 2023 · N407AS · Boeing 737900ER · Fuselage Miscellaneous Structure
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