Douglas DC-9-31

Service difficulty reports · 7,433

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC931'
  ORDER BY difficulty_date DESC"

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SDR USAA990505Clip · crackedPIT - DURING Q-4 CHECK, FOUND CRACKED ATTACH CLIP 1 INCH LONG AT STATION 965 LONGERON 17 LEFT. FABRICATED NEW CLIP. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990504Clip · crackedPIT - DURING Q-4 CHECK, FOUND TWO CRACKS APPROX 2 INCHES LONG ON SKIN FORMER CLIP AT STATION 965 RT, BETWEEN LONGERON 14R AND 16R. INSTALLED DOUBLER PER SRM 53-02 FIG 6 AND EA NR 52111. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990503Longeron · crackedPIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN LONGERON AT STATION 965 AT LONGERON 17L. SPLICED IN LONGERON PER SRM 53-22. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990502Longeron · crackedPIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN LONGERON AT STATION 980, LONGERON 17L. SPLICED IN LONGERON PER SRM 53-02. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990501Longeron · crackedPIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK AT LONGERON 9R CANTED STATION 1046. SPLICED IN LONGERON PER SRM 53-02 FIG 18. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990500Radial · crackedPIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK AT NR 2 RADIAL, APBH RIGHT SIDE, OUTBOARD END. COMPLETED CLIP REPAIR PER TYPICAL REPAIR 53-10-22. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990499Longeron · crackedPIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN LONGERON AT STATION 965, LONGERON 17 UPPER AND LOWER LEGS. INSTALLED SPLICE REPAIR PER SRM 53-04 FIG 18. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990498Skin · crackedPIT - DURING Q-4 CHECK, FOUND 1 INCH CRACK IN FUSELAGE SKIN AT STATION 963 LONGERON 16R. INSTALLED DOUBLER REPAIR PER SRM 53-04 FIG 31 AND EA 52111. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Main, Plate/SkinSDR USAA990497Frame · corrodedPIT - DURING Q-4 CHECK, FOUND 5 INCH BY 2 INCH CORROSION AT FRAME WEB AT STATION 996 FLOORBEAM WHERE IT ATTACHED TO RIGHT BELL FRAME. CORROSION LEVEL 1, CORROSION TASK NR C-57-533000. INSTALLED WEB AND FITTING AND DOUBLER PER EA 52122 AND SRM 53-05 FIG 72. Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Main, FrameSDR USAA990496Bulkhead · crackedPIT - DURING Q-4 CHECK, FOUND 2 INCH CRACK AT WEB AT STATION 965 BULKHEAD LOWER INBOARD CORNER. INSTALLED DOUBLER REPAIR PER SRM 53-03 FIG 21. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Main, BulkheadSDR USAA990495Frame · crackedPIT - DURING Q-4 CHECK, FOUND TWO CRACKS 1 INCH LONG ON FRAME AT SKIN CLIP STATION 945, LONGERON 14R TO 16R. MANUFACTURED NEW SKIN CLIP AND INSTALLED PER SRM 53-03 FIG 6. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Main, FrameSDR USAA990494Angle · crackedPIT - DURING Q-4 CHECK, FOUND 2.25 INCH CRACK AT ATTACH ANGLE AT STATION 965 BETWEEN 15R AND 16R. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990493Frame · crackedPIT - DURING Q-4 CHECK, FOUND .75 INCH LONG CRACK IN FRAME BETWEEN LONGERON 15 LT AND 16 LT AT STATION 965. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Main, FrameSDR USAA990492Longeron · crackedPIT - DURING Q-4 CHECK, FOUND TWO .5 INCH CRACKS AT LONGERON ATTACH POINTS, STATION 718 LONGERON 6 LT. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-02, FIG 18 SHEET 1. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990491Longeron · crackedPIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK AT LONGERON 2L, STATION 756. CUT OUT DAMAGED SECTION AND INSTALLED LONGERON REPAIR SECTION AND SPLICED PER SRM 53-02 FIG 18. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990490Longeron · crackedPIT - DURING Q-4 CHECK, FOUND .5 INCH CRACK AT LONGERON 5 LEFT, STATION 699. CUT OUT DAMAGED SECTION AND INSTALLED LONGERON REPAIR SECTION AND SPLICES PER SRM 53-02 FIG 18. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Main, Longeron/StringerSDR USAA990488Support · corrodedPIT - DURING Q-4 CHECK, FOUND 2 INCH BY 36 INCH CORROSION AT FLOOR SUPPORT MARKED NR 23 FORWARD GALLEY AREA, STATION 180. CORROSION LEVER 1. CORROSION TASK NR C46-53303. REMOVED, MANUFACTURED NEW FLOOR SUPPORT AND INSTALLED 7075T6 EXTRUSION C/C 1719673. (MJun 4, 1999 · N934VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990487Support · corrodedPIT - DURING Q-4 CHECK, FOUND CORROSION AT CUSP ANGLE (FLOOR SUPPORT) AT STATION 980-996, RT, L18. CORROSION LEVEL 1. CORROSION TASK NR C-58-53300. INSTALLED REPAIR PER SRM 53-05 FIG 25. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR USAA990486Cap · corrodedPIT - DURING Q-4 CHECK, FOUND CORROSION THE WHOLE WAY THROUGH END CAP, AT STATION 996 - LONGERON 19R. CORROSION LEVEL 1. CORROSION TASK NR C-57-53300. REWORKED AND REPLACED END CAP FITTING. (M)Jun 4, 1999 · N934VJ · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9900425Longeron · crackedDURING C-CHECK, FOUND LONGERON 17 LEFT CRACKED AT STATION 980. REPLACED LONGERON 17 LEFT IAW DC9 SRM 51-30-5.Jun 4, 1999 · N936AX · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA9900424Retainer · crackedDURING C-CHECK, FOUND WINDOW RETAINER CRACKED AT STATION 698, LEFT SIDE. REPAIRED IAW ABX REA D953-31670.Jun 4, 1999 · N936AX · Doug DC931 · Fuselage Miscellaneous StructureSDR ABXA9900423Pan · crackedDURING C-CHECK, FOUND AFT LOWER CARGO DOOR PAN CRACKED. REPLACED DOOR PAN IAW DC9 SRM 51-30-2.Jun 4, 1999 · N936AX · Doug DC931 · Cargo/Baggage DoorsSDR TWAA9908202Bulkhead Web · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION WITH POPPED RIVETS AND PILLOWING AT AFT PRESSURE BULKHEAD, STA 996 BETWEEN LONGERON 26L AND 28L. REMOVED CORROSION PER SPM 6-80-01 AND INSTALLED DOUBLER PER SRM 53-03, FIG 24.Jun 2, 1999 · N981Z · Doug DC931 · Fuselage Main, BulkheadSDR USAAD99071Light · dischargedPHL - THE GALLEY SERVICE DOOR EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE GALLEY SERVICE DOOR EMERGENCY LIGHT ASSEMBLY. (X)Jun 1, 1999 · N912VJ · Doug DC931 · Emergency LightingSDR TWAA9907904Skin · corrodedDURING OP 16 MAINT CHECK, FOUND SKIN CORROSION BEYOND LIMITS AT STA 756 TO 803, RBL 26L TO 26R. REPLACED SKIN PER DOUGLAS DRAWING 5911421 AND 5916154, AND SPM 6-70-01.May 28, 1999 · N981Z · Doug DC931 · Fuselage Main, Plate/SkinSDR TWAA9907708Longeron · crackedFOUND LONGERON 5L AT FS 699 CRACKED .25 INCH. FABRICATED AND INSTALLED LONGERON AND SPLICES IN LONGERON 5L AT FS 699 PER SRM 53-02 FIG 18 SHEET 1. CHECK-C 11-13-98 STL.May 28, 1999 · N977Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9907707Longeron · crackedFOUND LONGERON 4R AT FS 756 CRACKED .25 INCH. CUT OUT DAMAGED SECTION AND REPAIRED LONGERON PER SRM 53-02 FIG 18 SHEET 1. CHECK-C 11-13-98 STL.May 28, 1999 · N977Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9907706Longeron · crackedLONGERON 6R AT FS 756 WAS CRACKED .25 INCH. REPAIRED LONGERON 6R AT FS 756 PER SRM 53-02 FIG 18 SHEET 1. CHECK-C 11-13-98 STL.May 28, 1999 · N977Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9907703Longeron · crackedLONGERON 5L FS 639 WAS CRACKED .25 INCH. REPLACED SECTION ON LONG 5L AND INSTALLED SPLICE SECTION PER SRM 53-02, FIG 18 AND SRO9530128 DRAWING. CHECK-C 11-13-98 STL.May 28, 1999 · N977Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR ABXA9900385Controller · defectiveDURING CRUISE FLIGHT AT 310, A STRONG ACRID SMOKE ODOR AND WHIPSY SMOKE CAME FROM THE AUTOPILOT VERTICAL SPEED WHEEL. DECLARED EMERGENCY AND PERFORMED EMERGENCY CHECK LISTS. LANDED AT CLEVELAND HOPKINS AIRPORT WITHOUT INCIDENT. REPLACED THE AUTOPILOT CONTROMay 28, 1999 · N943AX · Doug DC931 · Autopilot SystemSDR TWAA9907705Longeron · crackedFOUND .25 INCH CRACKS AT LONGERON 6L AT FS 737 AND 756, AND LONGERON 7R AT FS 680. REPAIRED EACH PER SRM 53-02 FIG 18, AND SRO 9530128. CHECK-C 11-13-98 STL.May 27, 1999 · N977Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9907704Longeron · crackedLONGERON 6L AT FS 658 WAS CRACKED .25 INCH LONG. REPAIRED PER SRM 53-02, FIG 18 AND STANDARD PRACTICES. CHECK-C 11-13-98 STL.May 27, 1999 · N977Z · Doug DC931 · Fuselage Main, Longeron/StringerSDR TWAA9907903Support · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR SUPPORT AT STA 200. NUMBER 1 FLOOR TRACK TO MEMBRANE AREA, LBL 50. CORROSION WAS REMOVED PER SRM 6-80-01, PAGE 1 AND REPLACED FLOOR SUPPORT PER SPM 6-70-01.May 25, 1999 · N981Z · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9907902Floor · damagedDURING OP 16 MAINT CHECK, FOUND REPAIR ON FLOOR MEMBRANE BETWEEN STA 190 TO 210, LBL O IN TO 22 IN, WAS COMING LOOSE AND HAD POPPED RIVETS INSTALLED. REPLACED MEMBRANE PER SPM 6-70-01, 775T3 30 PER ORIGINAL SAMPLE.May 25, 1999 · N981Z · Doug DC931 · Fuselage Floor PanelSDR USAAD99069Switch · failedDAY-ROC - FLT 1743 - WHEN THE LANDING GEAR WAS LOWERED ON APPROACH THE NOSE GEAR UNSAFE RED LIGHT REMAINED ILLUMINATED. THE AIRCRAFT EXECUTED A GO-AROUND, AND AFTER SEVERAL MINUTES THE NOSE GEAR GREEN LIGHT ILLUMINATED AND THE RED UNSAFE LIGHT WENT OUT. THE May 24, 1999 · N978VJ · Doug DC931 · Landing Gear Position and WarningSDR GTIA9901019Panel · misalignedMHV - REPLACEMENT VERTICAL UPPER CENTER PANEL PN 9911940-403 ATTACH HOLES DO NOT ALIGN WITH AIRCRAFT STRUCTURE. FABED IN REF TO DC9 SRM 51-10 MANUFACTURED FOLLOWING ITEMS. 2 EACH CHANNELS 1 EA RT. 1 EACH LT. 2 INCH Z-CLIPS, 1 EACH RT, 1 EACH LT. 2 BULKHEAMay 24, 1999 · N934ML · Doug DC931 · Vertical Stabilizer, Plate/SkinSDR GTIA9901018Panel · crackedMHV - VERTICAL STABILIZER CENTER PANEL UPPER, PN 9911940-403, HAS CRACK RT AFT SIDE APPROXIMATELY 8 INCHES LONG. CENTER PANEL REPAIR AND INSTALLATION TO BE ACCOMPLISHED ON A092-A03-N065. (X)May 24, 1999 · N934ML · Doug DC931 · Vertical Stabilizer, Plate/SkinSDR GTIA9901011Panel · misalignedMHV - VERTICAL CENTER PANEL UPPER P/N 9911940-403 WHICH WAS REPLACED ON W/C NO062 HAS ATTACHING HOLES MISALIGNING WITH MATING HOLES ON VERT STRUT. PER ENG DWG NR 9909001 INSTALLATION COMPLETE PARTS FAB ON W/C A092-B10-N067 BRACKETS, CHANNELS, STRAPS ALL INSTAMay 24, 1999 · N934ML · Doug DC931 · Vertical Stabilizer, Plate/SkinSDR GTIA9901006Structure · damagedMHV - REMOVAL OF HORIZONTAL STABILIZER IS REQUIRED TO REPLACE WITH SERVICEABLE UNIT. REMOVED AND REPLACED HORIZONTAL STAB ASSY PER DC9 MM 55-10-0 PAGE 202. HORIZ STABILIZER ADJUSTMENT AND TEST C/W PER DC9 MM 55-10-0 PAGE 501 HORIZ STAB ACCESS PANELS WILL BE May 24, 1999 · N934ML · Doug DC931 · Horizontal Stabilizer StructureSDR GTIA9901026Floor · crackedMHV - CABIN CENTER RIGHT FLOOR PANEL STA 598 TO STA 639 HAS (5 EACH) CRACKS (3 EACH AT FASTENER HOLES AND TWO BELOW FASTENER HOLES). REPAIRED CRACKS INSTALLED DOUBLERS IAW SRM DC9 53-05 FAB DOUBLERS IAW SRM DC9 53-05 ALODINED AND PRIMED IAW SRM DC9 51-10-3. May 22, 1999 · N934ML · Doug DC931 · Fuselage Floor PanelSDR GTIA9901016Floorbeam · mismanufacturedMHV - BS 996 FLOORBEAM UPPER CAP ANGLE FROM LBL 12 TO EOP AT LBL 52 REQUIRES NEW SECTION TO ACCOMMODATE LT AFT LAV FLOOR STRUCTURE MOD. C/W ENGINEERING DWG NR 53-99197-2. ALODINED AND PRIMED. (X)May 22, 1999 · N934ML · Doug DC931 · Fuselage Main, Floor BeamSDR GTIA9901015Support · crackedMHV - CABIN CENTER LT FLOOR PANEL STA 579 TO STA 680 (BOTTOM OF FLOOR PANEL SUPPORT 2 AND 4 HAS CRACKS AND PUNCTURE HOLES). REMOVED SUPPORTS 2 AND 4 IAW SRM DC9 53-05 AND REPLACED SUPPORTS 2 AND 4 IAW SRM DC9 53-05. (X)May 22, 1999 · N934ML · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9901013Stringer · misdrilledMHV - PASSENGER CABIN INTERNAL STATION 550 TO 570 STRINGER L-17 THERE ARE APPROX 25 HOLES WITH SHORT C/C SPACING S/B .600 IAW SRM 53-02 FIG 18 SH 6 ARE .48-.58 REF NR A092-S03-W084. REMOVED AND REPLACED SKIN AND LONGERON SECTIONS FROM STATION 531 TO STATION 5May 22, 1999 · N934ML · Doug DC931 · Fuselage Main, Longeron/StringerSDR GTIA9901010Floor · wornMHV - LEFT CABIN FLOOR PANEL STATION 669 TO 775 SKIN AROUND NUMEROUS SCREW HOLES TO THIN. RESKINNED FLOOR PANEL IAW SRM DC9 53-20 AND 53-05, FABRICATED SKIN PANEL ALODINED AND PRIMED. (M)May 22, 1999 · N934ML · Doug DC931 · Fuselage Floor PanelSDR GTIA9901009Shear Tie · crackedREMOVED B/S REPAIR RT FUSE CRACK IN SHEAR TIE APPRON STATION 940 BETWEEN STRINGER 15/16. FABRICATED ANGLE DOUBLER PER DC9 IAW SRM 51-10-2 PAGE 1 FIG 2 PER SAMPLE SUPPLIED. (M)May 22, 1999 · N934ML · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9901004Intercostal · crackedMHV - PASSENGER CABIN INTERNAL STATION 484 LONGERON R-6 INTERCOSTAL CRACKED. REMOVED CRACK INTERCOSTAL AS REQUIRED TO FACILITATE FABRICATION OF REPLACEMENT PAR REF W/O A092-B03-W131 COPY ATTACHED INSTALLED REPLACEMENT AS REQUIRED PER DC9 SRM 51-30-5 AND 51-10May 22, 1999 · N934ML · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9900101Intercostal · crackedMHV - PASSENGER CABIN STATION 484 LONGERON R6 INTERCOSTAL CRACKED. FABRICATED REPLACEMENT ITEM REF DC9 SRM 51-10 HEAT TREAT NOT REQUIRED ISSUED TO AIRCRAFT FOR FIT AND INSTALL ON W/O A092B03W106. (M)May 22, 1999 · N934ML · Doug DC931 · Fuselage Miscellaneous StructureSDR GTIA9900100Intercostal · crackedMHV - PASSENGER CABIN INTERNAL STATION 484 LONGERON R-6 INTERCOSTAL CRACKED. REMOVED CRACK INTERCOSTAL AS REQUIRED TO FACILITATE FABRICATION OF REPLACEMENT PAR REF W/O A092-B03-W131 COPY ATTACHED INSTALLED REPLACEMENT AS REQUIRED PER DC9 SRM 51-30-5 AND 51-10May 22, 1999 · N934ML · Doug DC931 · Fuselage Miscellaneous StructureSDR TWAA9907501Power Supply · inoperativeDURING TAXI, FORWARD CABIN EGRESS LIGHTS CAME ON. AIRCRAFT RETURNED TO THE GATE. THE POWER SUPPLY WAS WORN OUT. POWER SUPPLY WAS REPLACED. CHECKS MADE TO ASSURE NORMAL OPERATION. CHECK -C 12-07-98 STL.May 21, 1999 · N993Z · Doug DC931 · Emergency LightingSDR GTIA9901024Longeron · crackedMHV - PASSENGER CABIN INTERNAL STA 560 LONGERON L-17 HAS A CRACK. HOLES WERE MIS-DRILLED. REPAIR WILL BE ACCOMPLISHED ON W/C NR A092-S39-W132. W132 - REMOVED AND REPLACED SKIN AND LONGERON SECTIONS FROM STA 531 TO STA 588, PRODUCTION SPLICE PER ENGINEERING May 21, 1999 · N934ML · Doug DC931 · Fuselage Main, Longeron/Stringer
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