Boeing 737-232

Service difficulty reports · 1,700

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 = '737232'
  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 NACA20100022Stringer Clip · crackedSTRINGER CLIP CRACKED AT FS 747, STRINGER 18R. REPLACED CRACKED STRINGER CLIP AT FS 747, STRINGER 18R. INSTALLED RIVETS AND HI-LOKS IAW B737 SRM 51-30-02. REPLACED PART PER 51-10-1 PARA 7.Nov 26, 2010 · N320DL · Boeing 737232 · Fuselage Main, Attach FittingsSDR NACA20100019Stringer Splice · corrodedCORRODED STRINGER SPLICE AT STA 907 STRINGER 27L AFT CARGO PIT. CORRODED STRINGER SPLICE AT STA 907 STRINGER 27L AFT CARGO PIT REPLACED. FABRICATED AND INSTALLED NEW PART IAW B737 SRM 53-10-2 PG 68C & 77. ALSO FABRICATED IAW 51-30-2 PG 1, 2, 3 AND 51-30-1 FNov 26, 2010 · N320DL · Boeing 737232 · Fuselage Main, Longeron/StringerSDR NACA20100024Intercostal · crackedFWD END OF INTERCOSTAL CRACKED AT FS 500, STRINGER 26L. CRACKED INTERCOSTAL REMOVED. FABRICATED NEW PART IAW BOEING DRAWING 69-41473 AND INSTALLED WITH NEW FASTENERS AT FS 500, STRINGER 26L IAW SRM 51-30-2, PARA 4 PG 2.Nov 24, 2010 · N320DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA20100018Beltframe · corrodedBELTFRAME TO SKIN CLIP CORRODED AT FS 947.5 BETWEEN STRINGERS 25L AND 24L. BELTFRAME TO SKIN CLIP AT STA. 947.5 BETWEEN STRINGER 25L AND 24L CORRODED BEYOND LIMITS. FABRICATED AND INSTALLED REPLACEMENT PART IAW B737 SRM 53-10-1 SECT 46 FIG 5 (SHEET 13) AND 5Nov 21, 2010 · N320DL · Boeing 737232 · Fuselage Main, FrameSDR NACA20100010Doubler · crackedFLOORBEAM DOUBLER CRACKED AT FS 680 RBL 24.8. WCS FLOORBEAM WEB CRACK WAS TRIMMED OUT AND REINFORCED. REPLACED CRACKED DOUBLER AND NEW UPPER CHORD CRACKS STOPPED DRILLED AND/OR REWORKED. FLOORBEAM DOUBLER AT FS 680 RBL 24.8 REPAIRED IAW 8100-9 REF ID 201011Nov 21, 2010 · N320DL · Boeing 737232 · Fuselage Main, Floor BeamSDR NACA20100009Doubler · crackedFLOORBEAM DOUBLER CRACKED AT FS 680 LBL 24.8. WCS FLOORBEAM WEB CRACK TRIMMED OUT AND REINFORCED. REPLACED CRACKED DOUBLER AND NEW UPPER CHORD CRACKS STOPPED DRILLED AND/OR REWORKED. FLOOR DOUBLER AT FS 680 LBL 24.8 REPAIRED IAW. 8100-9 REF: ID 201011290126Nov 21, 2010 · N320DL · Boeing 737232 · Fuselage Main, Floor BeamSDR NACA20100008Intercostal · crackedINTERCOSTALS CRACKED AT STRINGERS 7L, 10L, 13L AT BS 294.5 TO BS 303. REPLACED INTERCOSTAL AT STRINGERS 7L, 10L, 13L AT BS 294.5 TO BS 303 REPAIRED IAW CASTLE 8100-9 REF: ID 20101119088-0003D1 & CASTLE 8100-9 REF: ID 20101119088-0002D1.Nov 21, 2010 · N320DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA20100016Stringer · corrodedCORROSION ON STRINGER 27L JUST FWD OF BELTFRAME AT STA 1006 IN AFT CARGO COMPARTMENT EQUIPMENT BAY. CORROSION ON STRINGER 27L STA 1006 FOUND TO BE BEYOND ALLOWABLE LIMITS. REPLACED STRINGER SECTION IAW B737 SRM 53-10-3 FIG1 TYPE I.Nov 17, 2010 · N320DL · Boeing 737232 · Fuselage Main, Longeron/StringerSDR NACA20100015Stringer · corrodedCORROSION ON STRINGER 25L FS 992 IN AFT CARGO COMPARTMENT EQUIPMENT BAY. STRINGER 25L FS 992 IN AFT CARGO COMPARTMENT EQUIPMENT BAY CORROSION REMOVED AND DAMAGE FOUND OUT OF LIMITS PER 53-30-1 FIG. 1. REPAIRED STRINGER 25L FS 992 IAW B737 SRM 53-10-3 FIG 1 SNov 17, 2010 · N320DL · Boeing 737232 · Fuselage Main, Longeron/StringerSDR NACA20100014Intercostal · crackedCRACKED INTERCOSTAL AT FS 500A AFT SIDE, STRINGER 26L, FWD CARGO PIT. CRACKED INTERCOSTAL REMOVED. FABRICATED NEW PART IAW. BOEING DRAWING 69-41473 AND INSTALLED WITH NEW FASTENERS AT FS 500A, AFT SIDE, STRINGER 26L, FWD CARGO PIT IAW SRM 51-30-2 PARA 4, PGNov 16, 2010 · N320DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA20100013Intercostal · crackedCRACK IN FWD END OF INTERCOSTAL FS 440, STRINGER 25L, FWD CARGO PIT. CRACKED INTERCOSTAL REMOVED. FABRICATED NEW PART IAW BOEING DRAWING 69-41473 AND INSTALLED WITH NEW FASTENERS AT FS 440, STRINGER 25L, FWD CARGO PIT IAW SRM 51-30-2, PARA 4, PG 2.Nov 16, 2010 · N320DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA20100012Intercostal · crackedCRACK IN FWD END OF INTERCOSTAL FS 400 STRINGER 26L, FWD CARGO PIT. CRACKED INTERCOSTAL REMOVED. FABRICATED NEW PART IAW BOEING DRAWING 69-41473 AND INSTALLED WITH NEW FASTENERS AT FS 400, STRINGER 26L, FWD CARGO PIT IAW SRM 51-30-2 PARA 4, PG 2.Nov 16, 2010 · N320DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA20100011Attach Fitting · crackedATTACH CLIP AT AFT END OF INTERCOSTAL FS 500A L CRACKED, STRINGER 26 FWD CARGO PIT. CRACKED ATTACH CLIP REMOVED. FABRICATED NEW PART IAW BOEING DRAWING 69-41473 AND INSTALLED WITH NEW FASTENERS AT FS 500A, STR 26L, FWD CARGO PIT IAW SRM 51-30-2, PARA 4, PG 2Nov 16, 2010 · N320DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA20100005Line · leakingNR 2 ENGINE POWER LOSS, ENGINE SHUT DOWN. REMOVED PRESSURIZING & DUMP VALVE, REPLACED LEAKING LINE AND RE-INSTALLED P&D VALVE. OP & LEAK CHECK GOOD. REF: P&W MM 73-12-01.Aug 24, 2010 · N322DL · Boeing 737232 · Fuel Controlling SystemSDR NACA20100007Skin · crackedFUSELAGE SKIN HAS .25 INCH CRACK AT STA 932 STRINGER 22R.Aug 21, 2010 · N320DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA20100006Skin · crackedFUSELAGE SKIN HAS 2.6875 INCH CRACK AT STA 932 STRINGER 21R.Aug 21, 2010 · N320DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA20100004Bungee · brokenNOSE GEAR WOULD NOT EXTEND, LOSS OF HYDRAULIC QUANTITY, GEAR MANUALLY EXTENDED. FOUND BROKEN BUNGEE SPRING, BROKEN DOWN LINE AND DAMAGE TO BULKHEAD. REPLACED BUNGEE SPRING REF B737-200 MM 32-33-51, INSTALLED SERVICEABLE NOSE LANDING GEAR DOWN LINE REF B737-2Jul 12, 2010 · N321DL · Boeing 737232 · Landing Gear Retraction/Extension SystemSDR NACA20100003Fuse · brokenA SYSTEM HYDRAULIC QUANTITY LOSS. FOUND STUB LINE AT MAIN LANDING GEAR HYDRAULIC FUSE BROKEN. FABRICATED AND INSTALLED REPLACEMENT LINE AND PERFORMED LEAK CHECK WITH NO FURTHER DEFECTS NOTED. REF B737-200 MM 20-10-51 PAR 801.Jun 29, 2010 · N321DL · Boeing 737232 · Hydraulic System, MainSDR NACA20100002Skin · crackedFUSELAGE BELLY SKIN AT STA 520, BETWEEN STRINGERS 28L & 28R HAS A CRACK WHICH COMES OUT OF THE FORWARD L CORNER OF THE EXTERNAL AIR CONDITION ACCESS DOOR CUTOUT. PERFORMED HFEC AND SURFACE CONTOUR. CUT OUT, FABRICATED AND INSTALLED REPAIR DOUBLER .080 2024-T3Mar 3, 2010 · N322DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA20100001Window · crackedCAPTAINS SIDE WINDOW MULTIPLE CRACKS & FIRE (SPARKS). REPLACED L2 WINDOW. REF: B737-200 MM 56-12-11. CHECKED GOOD.Jan 31, 2010 · N322DL · Boeing 737232 · Flight Compartment WindowsSDR NACA20090014Filter · unknownNUBMER 1 "A" SYSTEM HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. NR 2 "A" SYSTEM LOW PRESSURE LIGHT ON/OFF INTERMITTENTLY. REMOVED NR 1 & 2 SYSTEM CASE DRAIN FILTERS, INSPECTED, NO CONTAMINATION NOTED. REPLACED WITH NEW FILTERS. OP & LEAK CHECK GOOD. PURGED Oct 20, 2009 · N322DL · Boeing 737232 · Hydraulic Reservoir, MainSDR NACA20090013Frame · crackedCRACKED FRAME AT BS 492 STR 22R RIGHT BELOW 40. REPLACED CRACKED FRAME AT BS 492 WITH P/N 65-20723-29 IAW DRAWING NR 65-20723, REV D AND 737-20 SRM 51-30-02.Mar 10, 2009 · N321DL · Boeing 737232 · Fuselage Main, FrameSDR NACA20090012Intercostal · crackedCRACK ON FWD ATTACH INTERCOSTAL STA 294 STR 7L. REPLACED INTERCOSTAL IAW B-737 SRM 51-10-01, SEC 7. FASTENERS INSTALLED IAW 51-30-02, INSTALLED INTERCOSTAL IAW KEL-NAC-09-0002-08B AND DRAWING 65C38823.Mar 10, 2009 · N321DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA20090011Stringer Clip · crackedCRACK ON AFT ATTACH CLIP OF INTERCOSTAL STA 360 STR 10L. REPLACED CRACKED ATTACH CLIP IAW B737 SRM 51-10-01. FASTENERS INSTALLED IAW 51-30-02. INSTALLED INTERCOSTAL IAW KEL-NAC-09-0002-08B, AND DRAWING 65C38823, STEP 3.Mar 10, 2009 · N321DL · Boeing 737232 · Fuselage Main, Attach FittingsSDR NACA20090010Stringer Clip · crackedBS 947 S26R CLIP CRACKED. FABRICATED AND REPLACED STRINGER CLIP AT STA 947 STR 26R WITH FABRICATED REPAIR PART IAW SRM 51-10-01, 51-20-01, 51-30-02, 51-10-02, 51-21-00.Mar 10, 2009 · N321DL · Boeing 737232 · Fuselage Main, Attach FittingsSDR NACA20090009Support Angle · crackedL1 DOOR OPENING SUPPORT ANGLE CRACKED AT STA 296, STRINGER 12L. REPLACED CRACKED SUPPORT ANGLE AT L1 DOOR OPENING AT STA 296, STRINGER 12L IAW SRM 51-10-01. FASTENERS INSTALLED IAW 51-30-02. INSTALLED ANGLE IAW KEL-NAC-09-0002-08, B AND DRAWING 65C38823.Mar 10, 2009 · N321DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA20090008Support Angle · crackedL1 DOOR OPENING SUPPORT ANGLE CRACKED AT STA 300 STRINGER 10L. REPLACED CRACKED SUPPORT ANGLE AT STA 300 STRINGER 10L IAW SRM 51-10-01 SECTION 7. FASTENERS INSTALLED IAW 51-30-02. INSTALLED ANGLE IAW KEL-NAC-09-0002-088, AND DRAWING 65C38823, STEP 4.Mar 10, 2009 · N321DL · Boeing 737232 · Fuselage Miscellaneous StructureSDR NACA20090007Skin · corrodedCORROSION ON SKIN FWD CARGO DOOR LOWER CUTOUT STA 480, STRINGER 23R. REPAIRED SKIN ON FWD CARGO LOWER CUTOUT STA 480, STRINGER 23R IAW SRM 53-30-03 DETAIL IV, CORROSION REMOVAL BEYOND LIMITS, MATERIAL REMOVED .059, MAXIMUM ALLOWABLE MATERIAL TO BE REMOVED .01Mar 2, 2009 · N321DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA20090006Stringer Splice · crackedSTRINGER CRACKED AT STA 540, STR. 10R. REPLACED CRACKED STRINGER SPLICE AT STA, 540, STR. 10R IAW B737 SRM 51-10-01 SECTION 7. FASTENERS INSTALLED IAW 51-30-02.Feb 26, 2009 · N321DL · Boeing 737232 · Fuselage Main, Longeron/StringerSDR NACA20090003Stringer Splice · crackedCRACK AT BS907 STR 4L STRINGER SPLICE. REPLACED STRINGER SPLICE AT BS907 STR 4L IAW SRM 51-10-01 SECTION 7. FASTENERS INSTALLED IAW 51-30-02.Feb 26, 2009 · N321DL · Boeing 737232 · Fuselage Main, Longeron/StringerSDR NACA20090004Skin · detachedLARGE GAP ON UNDERSIDE OF REPAIR AT STA 1016 BETWEEN STR 20R AND 21R. REPLACED WITH NEW REPAIR AT STA 20R-21R IAW B737 SRM PG.S 253-309 FIG. 48 DETAIL XXX.Feb 19, 2009 · N321DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA20090001Indicator · erraticABORTED TAKEOFF AT 70KTS FOR ERRATIC FIRST OFFICER AIRSPEED INDICATOR. REPLACED AIRSPEED INDICATOR AND TESTED.Feb 16, 2009 · N320DL · Boeing 737232 · Airspeed/Mach IndicatorSDR NACA20090005Door Frame · corrodedE AND E COMPARTMENT DOOR FRAME, RT SIDE, OTBD OF DOOR PIN STRUCTURE VERTICAL ANGLE CORRODED. REPLACED CORRODED ANGLE ON E AND E COMPARTMENT DOOR FRAME RT SIDE OTBD OF DOOR PIN STRUCTURE IAW SRM 51-10-01 SECTION 7. FASTENERS INSTALLED IAW 51-30-02.Feb 12, 2009 · N321DL · Boeing 737232 · Fuselage Main, StructureSDR CA081210005Cylinder · worn(CAN) RT MLG LOST FLUID. DURING ATTEMPTED SEAL CHANGE, THE INNER CYLINDER OF THE GEAR HAD A 6" BY 2" PIECE OF CHROME MISSING FROM THE INNER CYLINDER.Dec 9, 2008 · Boeing 737232 · Main Landing Gear Strut/Axle/TruckSDR KNN2008F00000Bolt · wornIN FLIGHT AGGRESSIVE VIBRATION FELT AT VARIOUS AIRSPEEDS 190 KTS-290 KTS, ALTITUDE STARTING AT 10,300 FT NOT RELENTING UNTIL WELL BELOW 190 KTS. (K)Aug 22, 2008 · N326DL · Boeing 737232 · Elevator Tab Control SystemSDR CA080829002Contactor · failed(CAN) AFTER LIFTOFF, SEVERAL FAILURES OCCURED. ANTISKID INOP, F/O PITOT INOP, NR2 EPR GUAGE INOP, NR2 AFT FUEL PUMP INOP, PINNED ASSOCIATED LIGHTS TO TRANSFER BUS PROBLEMS. LANDING BOTH 115V AND 28V AC TRANSFER BUS INOP. NR2 TRANSFER BUS CONTACTOR WAS FOUND TOAug 5, 2008 · Boeing 737232 · Electrical Power System WiringSDR NACA20080009Engine · out of trimNR 2 ENGINE NOT MAKING TAKEOFF THRUST. REJECTED TAKEOFF AT APPROXIMATELY 80 KNOTS. FOD INSPECTION COMPLETED WITH NO DEFECTS. FOUND ENGINES OUT OF TRIM. TRIMMED NR 1 AND NR 2 ENGINES BACMM 71-09-200. OPERATIONAL CHECKED GOOD.May 14, 2008 · N320DL · Boeing 737232 · Engine (Turbine/Turboprop)SDR NACA20080005Skin · crackedFUSELAGE SKIN CRACK AT STRINGER 24R STA 953 APPROXIMATELY 2 1/2" LONG. CRACK HAS BEEN TRIMMED OUT PER BOEING 737 SRM 53-30-03, FIG 48 TO 2,9375 INCH LONG AND .5625 INCH WIDE. LOCATED AT STR 24R, BS 953.125-BS 956.0625. INSTALLED REPAIR DOUBLER, TRIPLER, TEAMar 17, 2008 · N322DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA20080004Skin · crackedFUSELAGE SKIN CRACK AT STRINGER 23R STA 950 APPROXIMATELY 2 3/8" LONG. CRACK HAS BEEN TRIMMED OUT PER BOEING 737 SRM 53-30-03, FIG 48 TO 2,9375 INCH LONG AND .5625 INCH WIDE. LOCATED AT STR 23R, BS 950.75 - BS 953.6875. INSTALLED REPAIR DOUBLER, TRIPLER, TEMar 17, 2008 · N322DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR NACA20080003Skin · crackedFUSELAGE SKIN CRACKED AT STRINGER 21R, BS 931-BS 934.0625. CRACK IS 3.0625" LONG. REPAIRED PER BOEING REPAIR SKETCH AND SERVICE REQUEST MESSAGE 1-79197357-1 THRU -21, FAA FORM 8100-9, DATED 21 MARCH 2008. 8100-9 STATES ALTERNATE REPAIR HAS BEEN APPROVED AS Mar 17, 2008 · N321DL · Boeing 737232 · Fuselage Main, Plate/SkinSDR KNNA20080003Engine · failedACCORDING TO THE PILOT IN COMMAND’S REPORT, THEY HAD TO DEICE THE PLANE BEFORE TAKEOFF. THEN, ON TAKEOFF ROLL, DURING ROTATION, THERE WAS A LOUD BANG AND VIBRATION. THE CAPTAIN’S FIRST THOUGHT WAS THAT A TIRE HAD BLOWN. ONCE AIRBORNE, THE VIBRATION CONTINUEMar 8, 2008 · N326DL · Boeing 737232 · Engine (Turbine/Turboprop)SDR KNNA200700068Skin · damagedWHILE PERFORMING AN A-7 CHECK, A LIGHTNING STRIKE WAS FOUND ON THE LT ELEVATOR AT THE OUTBOARD TRAILING EDGE LOWER SIDE, UNDER I/B STATIC WICK, SPECIAL INSPECTION WAS PERFORMED IAW SKY KING GMM SECTION 4.03 AND AMM 05-51-151-201 WITH NO OTHER DAMAGE NOTED. ELDec 10, 2007 · N326DL · Boeing 737232 · Elevator, Plate/SkinSDR NACA20070021Door Frame · damagedDAMAGE TO MCD DOOR FRAME APPROXIMATELY 12-18 INCHES UP FROM AFT LOWER CORNER, MAIN CARGO DOOR AFT FRAME STA 500B+9 STRGR 15L-16L. HFEC AFFECTED AREA, NO FURTHER CRACKS. FABRICATED DOUBLERS AND REPAIRED PER NAC DRAWING NAC2007-320-02, FAA 8110-3 DATED 12-07-0Dec 7, 2007 · N320DL · Boeing 737232 · Fuselage Main, StructureSDR KNNA200700043Slat Track · jammedAFTER TAKEOFF, LT LEADING EDGE SLAT DID NOT RETRACT, AIRCRAFT DIVERTED FROM KGNV TO KJAX. PILOT DECLARED IN FLIGHT EMERGENCY FOR FLAPS UP LANDING. AFTER REMOVAL AND INSPECTION, FOUND OUTBD AUXILIARY TRACK JAMMED, WHICH CAUSED THE SLAT TO SHIFT AND THE TRAILINov 13, 2007 · N326DL · Boeing 737232 · Leading Edge DevicesSDR KNNA200700061Slat Track · jammedAFTER TAKEOFF, LT LEADING EDGE SLAT DID NOT RETRACT, AIRCRAFT DIVERTED FROM KGNV TO KJAX. PILOT DECLARED IN FLIGHT EMERGENCY FOR FLAPS UP LANDING. AFTER REMOVAL AND INSPECTION, FOUND OUTBD AUXILIARY TRACK JAMMED, WHICH CAUSED THE SLAT TO SHIFT AND THE TRAILINov 13, 2007 · N326DL · Boeing 737232 · Leading Edge DevicesSDR NACA20070019Actuator · fractured"A" SYSTEM HYDRAULIC FAILURE ON GROUND. REMOVED AND REPLACED NR 8 SPOILER ACTUATOR DUE TO HOUSING FAILURE. LEAK CHECK, FUNCTIONAL CHECK AND SPOILER TO FLAP CLEARANCE CHECKED GOOD. REF: B737MM 27-62-101.Sep 23, 2007 · N321DL · Boeing 737232 · Drag Control ActuatorSDR KNNA200700041Hose · leakingWHILE EN ROUTE TO ATLANTA HARTSFIELD AIRPORT (KATL) FROM TUNICA, MISSISSIPPI (KUTA) AS SKY KING FLT (SGB332) THE CREW NOTICED A SLOW LOSS OF SYSTEM “A” HYDRAULIC FLUID. AFTER DECLARING AN IN-FLIGHT EMERGENCY, AN UNEVENTFUL LANDING WAS MADE, THE CREW TAXI THE Sep 2, 2007 · N332D · Boeing 737232 · Hydraulic System, MainSDR KNNA200700030Lever · bindingIN FLIGHT DURING DESCENT INTERMITTENTLY AT FIRST THEN STEADY PROCEDURES WERE FOLLOWED WITH THRUST LEVERS BINDING (RESTRICTED) ENGINE 1 WAS SHUTDOWN IAW CHECK LIST. EMERGENCY DECLARED. THRUST REVERSER WAS TRANSFER TO DMI LOG TROUBLESHOOTING IS IN PROCESS.Apr 28, 2007 · N326DL · Boeing 737232 · Engine Thrust ReverserSDR KNNA200700022Floorbeam · corrodedFLOOR PANEL ATTACH POINT STA 344, LBL 12 IS CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF STA 344, LBL 12 FLOOR PANEL ATTACH POINT. REMOVED AND REPLACED FLOORBEAM SRM 53-10-9 FIG 6.Mar 14, 2007 · N326DL · Boeing 737232 · Fuselage Main, Floor BeamSDR KNNA200700026Frame · damagedAFT CARGO PIT, INTERIOR BILGE B-STA 867 BETWEEN STR 27 R AND STR 28 L FRAME BOTTOM SIDE, CORRODED. PROVIDE INSTRUCTIONS ON REPAIR OF CORROSION AFT CARGO PIT, INTERIOR BILGE BS 867 BETWEEN STR 27R-27L BOEING SRM 53-10-4 FIGURE 7.Mar 11, 2007 · N326DL · Boeing 737232 · Fuselage Main, Frame
Back to Boeing 737-232