Douglas DC-9-32

Service difficulty reports · 12,755

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'DC932'
  ORDER BY difficulty_date DESC"

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SDR AT9900201Fitting · damageSCHEDULED INSPECTION AT AEROCORP, FL. FOUND THE FORWARD CARGO DOOR LATCH SUPPORT FITTING REQUIRED REPLACEMENT. INSTALLATION OF THE NEW FITTING REQUIRED TRIMMING OF THE DOOR INNER SKIN AROUND ONE OF THE LIGHTENING HOLES. THE BEADED FLANGE AT THE LOWER CORNERMar 9, 1999 · N821AT · Doug DC932 · Cargo/Baggage DoorsSDR AT9900190Cover · looseFOUND DURING PREFLIGHT CHECK, THE L-1 DOOR SLIDE COVER LOOSE. RESECURED THE L-1 DOOR SLIDE COVER IAW MM 25-62. RII ACCOMPLISHED.Mar 9, 1999 · N811AT · Doug DC932 · Emergency EquipmentSDR AT9900183Doubler · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND CORROSION ON THE FRONT FACE OF CANTED WEB AT BS 1046.376. FABRICATED DOUBLER, ALODINE, PRIMED, AND INSTALLED REPAIR IAW DC9 SRM 53-01-0, AND 53-10-3.Mar 9, 1999 · N822AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900182Lever · out of adjustON CLIMB, GEAR LEVER WILL NOT RAISE, AIR RETURN. RIGGED LANDING GEAR CONTROL LEVEL ANTI-RETRACTION LATCH IAW DC9 MM 32-31-1. CHECKED RIG ON GROUND SENSE CONTROL, MECHANICAL RIG CHECK GOOD IAW DC9 MM 32-23-1.Mar 9, 1999 · N815AT · Doug DC932 · Landing Gear SelectorSDR 9900899919Wire · failedEN ROUTE MSP-IAD, C PHASE OF LEFT GENERATOR BUS CIRCUIT BREAKERS POPPED FOLLOWED BY ALL ROW H FUEL PUMP CIRCUIT BREAKERS. CREW DECLARED AN EMERGENCY AND FLIGHT WAS DIVERTED TO IND. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED CIRCUIT BREAKER B1-27Mar 9, 1999 · N941N · Doug DC932 · AC Generation SystemSDR AT9900210Angle · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND CORROSION AROUND FASTENER HEADS ON ATTACH ANGLE AND WEB (TOP SIDE) AT BS 130 LBL 54 ON THE E/E BAY CEILING. REMOVED CORROSION AROUND FASTENER HEADS, FABRICATED REPAIR DOUBLER, LOCATED AND DRILLED, TREATED, PRIMED, Mar 8, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR ABXA9900191Latch · brokenCOCKPIT DOOR WOULD NOT OPEN. REPAIRED COCKPIT DOOR LATCH.Mar 8, 1999 · N928AX · Doug DC932 · Fixed Inner DoorsSDR 9900949610Frame · crackedDURING PERIODIC CHECK, FOUND FRAME UNDER AIRSTAIR TORQUE TUBE CRACKED IN AFT ACCESSORY COMPARTMENT. BRACKET TO FRAME WAS ALSO BROKEN. INSTALLED REPAIR PER EA 96-165737.Mar 8, 1999 · N610NW · Doug DC932 · Fuselage Main, FrameSDR 9900939610Frame · crackedDURING PERIODIC CHECK, FOUND FRAME CRACKED IN RADIUS; BOTTOM OF CANTED FRAME AT FS 1143. INSTALLED REPAIR PER EA 96-165739.Mar 8, 1999 · N610NW · Doug DC932 · Fuselage Main, FrameSDR TWAA9903815Skin · corrodedDURING OP 15 MAINT CHECK, FOUND FUSELAGE SKIN CORRODED UNDER PREVIOUSLY INSTALLED REPAIR DOUBLER BETWEEN STA 569 AND 579, LONGERON 29L TO 29R. REMOVED CORROSION PER SPM 6-80-01. REPAIRED PER SRM 53-04, FIG 43.Mar 7, 1999 · N923L · Doug DC932 · Fuselage Main, Plate/SkinSDR AT9900300Cargo Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD PIT CARGO TIE DOWN TRACK CORRODED ON BACK SIDE. REMOVED AND REPLACED TRACK IAW DC9 SRM 53-21-0.Mar 7, 1999 · N822AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900194Spar · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND REAR SPAR LOWER CHORD AFT TANG HAS A CRACK INDICATION AT INBOARD BUTE DOOR THIRD HOLE FROM OUTBOARD END. STEPPED UP HOLE TO .437, FABRICATED AND INSTALLED BUSHING IAW DC9 SRM 51-10-3 AND SB 57-150 RZMar 7, 1999 · N813AT · Doug DC932 · Wing SparSDR TWAA9903814Seat Track · corrodedDURING OP 15 MAINT CHECK, FOUND CORROSION ON CHAIR TRACK RBL 22 AT STA 200 TO 315. REPLACED TRACK FROM STA 200 TO STA 315 PER SRM 53-05, FIG 4.Mar 5, 1999 · N923L · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9903604Longeron · crackedDURING OP 15 MAINT CHECK, FOUND LONGERON 16L CRACKED AT STA 965. CONFIRMED BY NDT. REPAIRED CRACKED LONGERON 16L AT STA 965 PER SRM 53-02, FIG 18, PER PAGE 1 PARAGRAPH B.Mar 5, 1999 · N923L · Doug DC932 · Fuselage Main, Longeron/StringerSDR MWEA99084Cover · detachedTHE GALLEY SLIDE COVER FELL OFF. MTC REATTACHED THE GALLEY SLIDE COVER.Mar 5, 1999 · N216ME · Doug DC932 · Emergency EquipmentSDR AT9900179Battery · dischargedEMERGENCY LIGHTING AFT CABIN CEILING BY AFT DOOR DID NOT ILLUMINATED BRIGHTLY. CHARGED BATTERIES IAW 33-53-0, OPERATIONAL CHECK GOOD.Mar 5, 1999 · N835AT · Doug DC932 · Emergency LightingSDR AT9900178Wire · out of positionEMERGENCY LIGHTING IN COCKPIT DID NOT ILLUMINATE. REPOSITIONED WIRING ON CONNECTOR IN FORWARD AISLE LIGHTING RECEPTICAL. OPERATIONAL CHECKS GOOD IAW DC9 STANDARD PRACTICES CHAPTER 20-50.Mar 5, 1999 · N835AT · Doug DC932 · Light System WiringSDR GTIA990925Support · corrodedMHV - FLOOR SUPPORT AT STATION 220 RBL 48 TO RBL 56 IS SEVERELY CORRODED. REMOVED FLOOR SUPPORT FOR FURTHER INSPECTION FOUND TO BE OUT OF LIMITS PER 51-10-3. FABRICATED NEW SUPPORT PER DC9 SRM 51-10-1 SURFACE TREATMENT AND INSTALLED NEW SUPPORT PER DC9 SRM 5Mar 4, 1999 · N13512 · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9900218Skin · crackedINSPECTION FOUND A 2 INCH CRACK AND SEVERAL LOOSE RIVETS IN RT SIDE OF RUDDER UPPER SKIN. THE EFFECTED AREA OF SKIN WAS REMOVED AND A NEW SECTION OF SKIN WAS INSTALLED IAW SRM 55-03-00, FIGURE 12, PAGE 19.Mar 4, 1999 · N17557 · Doug DC932 · Rudder, Plate/SkinSDR TWAA9903606Bolts · rustedDURING OP 15 MAINT CHECK, FOUND 4 I/B AFT FLAP CASTING ATTACH BOLTS ON REAR SPAR EMITTING RUST. REPLACED STUDS AND HINGE FITTING PER MM 57-40-0 AND 27-51-1.Mar 3, 1999 · N923L · Doug DC932 · Trailing Edge FlapsSDR TWAA9903605Former · crackedDURING OP 15 MAINT CHECK, FOUND LOWER FLANGE OF FORMER RING CRACKED AND DAMAGED AT STA 218, LONGERON 19L, AT FORMER TO LONGERON. REPAIRED FORMER RING PER SRM 53-03, PAGE 4A, FIG 2A.Mar 3, 1999 · N923L · Doug DC932 · Fuselage Main, FrameSDR TWAA9903603Fitting · corrodedDURING OP 15 MAINT CHECK, FOUND SHIP DRAIN FITTING AT STA 550 BETWEEN LONGERONS 29L AND 30, WITH CORROSION. REPLACED DRAIN FITTING WITH (P/N 17-52804) AND FASTENERS PER SRM 51-30-0.Mar 3, 1999 · N923L · Doug DC932 · Fuselage Miscellaneous StructureSDR GTIA9900033Light · miswiredDTW - EMERGENCY LIGHTS AT ROW 17 AND 18 WON'T LIGHT, OVERHEAD. UNCROSSED EMERGENCY AND STANDBY LIGHT WIRES. OPERATION CHECK GOOD IAW DC-9 MM 33-50-0. (M)Mar 3, 1999 · N12505 · Doug DC932 · Emergency LightingSDR AT9900282Cargo Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT TRACK CORRODED ON THE BOTTOM SIDE. FABRICATED, LOCATED, DRILLED, DEBURRED, COUNTERSUNK, PRIMED, TREATED, AND INSTALLED IAW DC9 SRM 53-05 FIG 4C, 51-10-3 AND 51-10-4.Mar 3, 1999 · N813AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900277Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE AFT PIT RIGHT SIDE FLOOR TRACK CORRODED ON BOTTOM FULL LENGTH. FABRICATED, DRILLED, DEBURRED, PRIMED, AND TREATED IAW DC9 SRM 53-05 FIG 4C, 51-10-4, AND 51-10-3.Mar 3, 1999 · N813AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900214Thrust Reverser · chafedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND ON THE NR 1 ENGINE THRUST REVERSER AT THE FORWARD MATING FLANGE TO THE ENGINE COWLING WITH A CHAFED AREA APPROXIMATELY FIVE INCHES LONG THRU THE BASE OF THE METAL. CUT OUT CHAFED AREA, FABRICATED, FORM FILLER AND Mar 3, 1999 · N815AT · Doug DC932 · Engine Thrust ReverserSDR AT9900180Angle · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND A CRACK IN VERTICAL LEG OF NR 2 PYLON UPPER ATTACH ANGLE AT BS 980. STOP DRILLED CRACK, HIGH FREQUENCT EDDY CURRENT VERIFIED CRACK WAS STOP, FABRICATED AND INSTALLED REPAIR IAW DC9 SRM 51-30-2, AND RES NR 99442.Mar 3, 1999 · N815AT · Doug DC932 · Fuselage Miscellaneous StructureSDR 9900909985Web · crackedDURING PERIODIC CHECK, FOUND WEB CRACKED AT FS 148 ABOVE LONGERON 27L AT FORWARD E/E COMPARTMENT. INSTALLED REPAIR PER EA 99-163382.Mar 3, 1999 · N985US · Doug DC932 · Fuselage Miscellaneous StructureSDR CALA9900209Wire · brokenINSPECTION FOUND THE OVERHEAD EMERGENCY LIGHT AT ROW 10 INOPERATIVE. MAINTENANCE FOUND LIGHT WIRE PULLED FROM SPLICE. THE WIRE WAS RESPLICED AND OPERATION CHECKED GOOD.Mar 2, 1999 · N14524 · Doug DC932 · Light System WiringSDR CALA9900208Batteries · dischargedINSPECTION FOUND BOTH NACELLE EMERGENCY LIGHTS INOPERATIVE. THE BATTERIES WERE REMOVED AND REPLACED AND OPERATION CHECKED GOOD.Mar 2, 1999 · N14524 · Doug DC932 · Emergency LightingSDR AT9900276Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT RIGHT HAND TRACK BOTTOM SIDE CORRODED THROUGHOUT. REMOVED CORROSION, LOCATED NEW TRACK, DRILLED, COUNTERSUNK, DEBURRED, TREATED, AND PRIMED IAW DC9 SRM 53-05 FIG 4C, 51-10-4, AND 51-10-3.Mar 2, 1999 · N813AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900217Web · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND FLOOR WEB AT BS 617 CRACKED. FORMED DOUBLERS, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED REPAIR AND REINSTALLED TWO PREVIOUSLY REMOVED BAFFLES IAW DC9 SRM 51-10-4, 53-20-1, 51-10-3, 51-30-2, AMar 2, 1999 · N821AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900196Web · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE LEFT HAND FLOOR WEB AT BS 617 CRACKED. FORMED DOUBLERS, DRILLED, DEBURRED, TREATED, PRIMED, AND COMPLIED WITH RES NR 99358. REINSTALLED REMOVED BAFFLES, AND INSTALLED REPAIR IAW DC9 SRM 51-10-3, 53-20-1, 51-3Mar 2, 1999 · N821AT · Doug DC932 · Fuselage Miscellaneous StructureSDR MWEA99082Slide · detachedBDL - FLT 49 - THE GALLEY DOOR SLIDE CAME OUT OF COVER. MTC REINSTALLED GALLEY DOOR SLIDE. (X)Mar 1, 1999 · N216ME · Doug DC932 · Emergency EquipmentSDR CALA9900207Batteries · dischargedINSPECTION FOUND THE TAIL CONE EMERGENCY EXIT FLOOD LIGHT INOPERATIVE. THE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD.Mar 1, 1999 · N14524 · Doug DC932 · Emergency LightingSDR AT9900209Floorbeam · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FLOORBEAM UPPER CAP CORRODED AROUND FASTENER HOLES AT BS 980 RBL 38 TO 42. REMOVED, FIT, TRIMMED, DRILLED, AND INSTALLED UPPER CAP REPAIR ANGLE IAW DC9 SRM 51-10-3, 53-01 FIG 1, 53-05 FIG 20A, 51-10-4, 51-30-2,Mar 1, 1999 · N813AT · Doug DC932 · Fuselage Main, Floor BeamSDR CALA9900205Rib · crackedINSPECTION FOUND A 1.5 AND 2 INCH CRACK IN NOSE RIB AT HI-LOK INSIDE RT WING FIXED LEADING EDGE I/B OF NR 5 SLAT CENTER TRACK. THE RIB WAS REMOVED AND A NEW RIB REPAIR WAS INSTALLED IAW SRM 57-01, PAGE 9.Feb 28, 1999 · N17557 · Doug DC932 · Wing, Rib/BulkheadSDR CALA9900204Bracket · crackedINSPECTION FOUND BRACKET CRACKED THROUGH AND A 2 INCH CRACK AT SPLICE INSIDE LT WING FIXED L/E AT JOINT BETWEEN NOSE RIBS, TEN INCHES O/B OF NR 2 SLAT O/B TRACK, XRS 254. AN ANGLE AND STRAP WERE INSTALLED IAW SRM 51-10-2, 51-00-00, 51-10-3, 51-30-2, AND 51-30Feb 28, 1999 · N17557 · Doug DC932 · Wing Miscellaneous StructureSDR GTIA9900924Skin · damagedMHV - FS 218 264 LONGERON 15-18 SKIN REPAIR DAMAGED LEFT SIDE. REPLACED DAMAGED SKIN AND FINGER DOUBLERS PER DWG 53-99034 FAX SURFACED SEAL ALL PARTS PER 51-20-0. INSTALLED FASTENERS WET WITH PR1422-B2. INSTALLED HI-LOCKS PER SRM 51-30-5 AND SOLID RIVETS PEFeb 27, 1999 · N13512 · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900280Floor · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD PIT CENTER FLOOR PANEL CORRODED ALONG THE EDGES AND ELONGATED HOLES WITH NO EDGE DISTANCE. FABRICATED REPAIR FLOOR PANEL, LOCATED, DRILLED, DEBURRED, TREATED AND PRIMED IAW DC9 SRM 51-10-3, 53-01 FIG 1, Feb 27, 1999 · N813AT · Doug DC932 · Fuselage Floor PanelSDR AT9900151Wire · brokenFLIGHT ATTENDANT REPORTED ELECTRICAL SMELL IN THE CABIN AFTER TAKEOFF. RETURNED TO GATE IN ATLANTA. CABIN WARNING SIGN POPS CIRCUIT BREAKER. REPAIRED BROKEN WIRE ON AFT LAVATORY RETURN TO CABIN SIGN IAW MM 33-21. ALL SYSTEMS CHECKED GOOD.Feb 27, 1999 · N818AT · Doug DC932 · Light System WiringSDR TWAA9903701Skin · damagedDURING OP 15 MAINT CHECK, FOUND FUSELAGE SKIN DAMAGED AT STA 37, 3 O'CLOCK POSITION, AND INTERIOR STRUCTURE DAMAGED AND CRACKS AT ALIGNMENT PINS. REPAIRED SKIN AND STRUCTURE PER ARA 16069 AND 16068. CRACK REPAIRED PER SPM 6-70-01.Feb 26, 1999 · N923L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9903403Casting · crackedDURING OP 15 MAINT CHECK, FOUND FUSELAGE FORMER CASTING CRACKED AT STA 718, AND SIDE BRACE HOLES CORRODED AT STA 718. REPLACED CASTING AT STA 718 PER ARA 16061, AND OVERSIZED SIDE BRACE HOLES PER ARA 16063 AND SPM 6-80-01.Feb 26, 1999 · N923L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9903402Support · corrodedDURING OP 15 MAINT CHECK, FOUND FLOOR SUPPORT AT STA 160 TO 266, RBL 44 TO 54, WAS CORRODED. FABRICATED NEW SUPPORT, TREATED, PRIMED AND PAINTED PART AND AREA. INSTALLED SUPPORT PER SPM 6-80-01.Feb 26, 1999 · N923L · Doug DC932 · Fuselage Main, Floor BeamSDR GTIA9900920Web · gougedREF PO88 - GOUGE ON SHEAR WALL WEB .010 DEEP MATERIAL .032 BEYOND LIMITS STATION 965 SBL. REMOVED DAMAGED WEB AND REPLACED WITH NEW 991224-3 WEB INSTALLED FASTENERS PER DC9 SRM 51-30-1 FOR BOLTS 51-30-5 FOR HI-LOCKS 51-30-2 RIVETS. (M)Feb 26, 1999 · N13512 · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900292Support · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CABIN FLOOR SUPPORT CORRODED ON THE UPPER SURFACE AND ON BOTTOM OF UPPER FLANGE AROUND CLIP NUTS AT BS 157 TO 218. REMOVED CORROSION, FABRICATED REPAIR ANGLE, DRILLED, DEBURRED, TREATED, PRIMED AND INSTAFeb 26, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900281Seat Track · corrodedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE FORWARD CABIN SEAT TRACK AT BS 200 TO 279 RBL 22 CORRODED. REMOVED FLOOR PANELS, FABRICATED NEW SEAT TRACK AND SPLICE, LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED IAW DC9 SRM 53-05 FIG 4, 51-10-3, 51-30-1, Feb 26, 1999 · N813AT · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR AT9900208Support · corrodedSCHEDULED INSPECTION AT AERO CORP, FL, FOUND THE FORWARD CABIN FLOOR SUPPORT CORRODED AND PART OF UPPER FLANGE HAS BEEN PREVIOUSLY REMOVED AT BS 210 TO 237 LBL 16. REMOVED FLOOR SUPPORT, FABRICATED NEW SUPPORT, ALODINED, PRIMED, AND INSTALLED IAW DC9 SRM 53-1Feb 26, 1999 · N813AT · Doug DC932 · Fuselage Miscellaneous StructureSDR AT9900164Skin · crackedFOUND A CRACK IN SKIN OF RUDDER APPROXIMATELY AT STATION ZR 70, CRACK IS ABOUT SEVEN INCHES LONG RUNNING PARALLEL WITH RIBS. STOP DRILLED FORWARD END OF CRACK IAW RES NR 99541, AFT END OF CRACK TERMINATES AT A RIVET HOLE. APPLIED SPEED TAPE TO CRACK IAW RES Feb 26, 1999 · N809AT · Doug DC932 · Rudder, Plate/SkinSDR AT9900152Valve · defectiveLOST CABIN PRESSURE, UNABLE TO CONTROL IT MANUALLY. PASSENGER IN AFT CABIN REPORTED HEARING A POP JUST BEFORE THE MASK DROPPED. FOUND THE AFT CABIN PRESSURE SAFETY VALVE OFF IT'S SEAT. REMOVED AND REPLACED SAFETY VALVE PRESSURE IAW MM 21-30, OPS CHECKED GOOFeb 26, 1999 · N839AT · Doug DC932 · Cabin Pressure Control System
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