N9305N, cancelled May 21, 2007

Service difficulty reports · 50

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N9305N' AND deregistration_id = 'N9305N-2007-05-21'
  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 AALA20040847Connector · shortedINFLIGHT T1261 DFW SAT/14 AT 26,000 FEET LEVEL GOT AN INDICATION OF AFT CARGO FIRE. FOLLOWED QRH AND BOTH BOTTLES FIRED. LANDED WITHOUT INCIDENT. REPLACED NR 1 AND 2 CARGO BOTTLES. REPLACED COCKPIT CONTROL AND CONTROL PANEL. FOUND CONNECTOR SHORTED OUT ON AAug 14, 2004 · N9305N · Doug DC983 · Electrical ConnectorsSDR ZW0A0212902Valve · defectiveNOSE GEAR STRUT FLAT NOT ALLOWING GEAR TO RETRACT. REMOVED AND REPLACED SCHRADER VALVE AND RESERVICED STRUT.Dec 26, 2002 · N9305N · Doug DC983 · Nose/Tail Landing Gear Strut/AxleSDR ZW0A0212801Seal · looseBOTH HEAT EXCHANGERS LEAKING NOT ALLOWING AIRCRAFT TO PRESSURIZE. TIGHTENED SEALS ON BOTH HEAT EXCHANGERS.Dec 23, 2002 · N9305N · Doug DC983 · Cabin Cooling SystemSDR ZW0A0210401Power Supply · dischargedTHE EGRESS LIGHTING BETWEEN ROWS 15 TO 21 WERE FLASHING ON AND OFF DURING FLIGHT. REPLACED THE POWER SUPPLY.Oct 8, 2002 · N9305N · Doug DC983 · Emergency LightingSDR ZW0A0206201Fitting · crackedDURING CHECK-C MAINT THE FORMER FOOT WAS CRACKED AT STA 1361 BETWEEN LONGERON 23L AND 24L. FABRICATED AND INSTALLED NEW FORMER FOOT SECTION PER SPM 6-70-01, PAGE 2 AND 3, ITEM 4. FABRICATED AND INSTALLED PER SRM 51-30-02 AND 51-30-5.Jun 11, 2002 · N9305N · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0206003Floorbeam · damagedDURING CHECK-C MAINT THE FLOOR BEAM CAP WAS GROUND BEYOND LIMITS AT STA 1322, LBL 34. REPAIRED FLOOR BEAM CAP PER SRM 53-05, FIG 20A.Jun 5, 2002 · N9305N · Doug DC983 · Fuselage Main, Floor BeamSDR ZW0A0205902Tie Clip · crackedDURING CHECK-C CRACKED TIE CLIP AT STA 1437 VERT BULKHEAD TO LONG 3R. REPLACED TIE CLIP PER SPM 6-70-01.Jun 4, 2002 · N9305N · Doug DC983 · Fuselage Miscellaneous StructureSDR ZW0A0205303Floorbeam · corrodedDURING CHECK-C MAINT FOUND CORROSION IN LATERAL FLOOR BEAM AT STA 180, FROM RBL 8 TO RBL 43. FABRICATED AND INSTALLED FLOOR SUPPORT PER SRM 51-01, PAGE 1 ITEM C.May 22, 2002 · N9305N · Doug DC983 · Fuselage Main, Floor BeamSDR ZW0A0205302Stringer · crackedDURING CHECK-C MAINT STRINGER 3 LT WAS CRACKED AT STA 160, ABOVE ELECT PANEL. REPAIRED LONGERON 3 PER SRM 53-02, FIG 18.May 17, 2002 · N9305N · Doug DC983 · Fuselage Main, Longeron/StringerSDR ZW0A0205301Door Frame · crackedDURING CHECK-C MAINT THE RT FWD GALLEY SERVICE DOOR HAD A CRACKED DOUBLER LOWER HINGE ARM. REPLACED WITH NEW FRAME PART PER SPM 6-70-01.May 17, 2002 · N9305N · Doug DC983 · Service DoorsSDR ZW0A0205203Longeron · crackedDURING CHECK-C MAINT THE NUMBER 4 LT LONGERON WAS CRACKED AT STA 160. REPLACED DAMAGED SECTION OF LONGERON PER SRM 53-02, FIG 18.May 16, 2002 · N9305N · Doug DC983 · Fuselage Main, Longeron/StringerSDR ZW0A0111203Wire · brokenDURING PREFLIGHT INSPECTION IT WAS NOTED THE RH MID ZONE EGRESS LIGHTS WERE INOP. REPAIRED BROKEN WIRE AT ROW 16 RH SIDE.Nov 25, 2001 · N9305N · Doug DC983 · Light System WiringSDR ZW0A011123Wire · brokenDURING PREFLIGHT INSPECTION IT WAS NOTED THE RH MID ZONE EGRESS LIGHTS WERE INOP. REPAIRED BROKEN WIRE AT ROW 16 RT SIDE.Nov 25, 2001 · N9305N · Doug DC983 · Light System WiringSDR ZW0A0107502Battery PackTHE CABIN OVERHEAD EMERGENCY LIGHTS ILLUMINATED WHEN POWER WAS REMOVED FROM THE AIRCRAFT. REPLACED THE BATTERY PACK. CHECK-C 5-7-01 STL. --CLOSED--Aug 25, 2001 · N9305N · Doug DC983 · Emergency LightingSDR ZW0A0107101LampDURING LANDING THE RIGHT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE, DUE TO BURNED OUT BULB. REPLACED LIGHT BULB P/N 387.LAST CHECK C 05/07/01 STL. --- CLOSED ---Aug 17, 2001 · N9305N · Doug DC983 · Landing Gear Retraction/Extension SystemSDR ZW0A0106303Battery Pack · dischargedDURING MAINTENANCE THE AFT FLOOR EGRESS LIGHTS WERE INOP DUE TO WEAR. REPLACED BATTERY PACK P/N5822-2 AND FEEDER JUMPER CABLE PER MM 33-51-01.Aug 4, 2001 · N9305N · Doug DC983 · Emergency LightingSDR ZW0A0103202Battery Pack · dischargedIN FLIGHT THE EGRESS LIGHTS AT ROWS 15 TO 22 ILLUMINATED. REPLACED THE BATTER PACK. CHECK-C 5-7-01 STL.Jun 8, 2001 · N9305N · Doug DC983 · Emergency LightingSDR ZW0A0102705Power Supply · dischargedAN OVERWING EMERGENCY EXIT LIGHT REMAINED ON IN FLIGHT. REPLACED THE POWER SUPPLY. CHECK-C 5-7-01 STL.Jun 2, 2001 · N9305N · Doug DC983 · Emergency LightingSDR ZW0A0102302Battery · dischargedTHE EGRESS LIGHTING IN THE FIRST CLASS CABIN WAS INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 5-7-01 STL.May 24, 2001 · N9305N · Doug DC983 · Emergency LightingSDR TWAA0106301Wire · brokenTHE AFT CABIN EXIT IDENTIFIER FAILED TO ILLUMINATE. REPAIRED A BROKEN WIRE IN CEILING OF AFT LEFT LAVATORY. CHECK-C 2-5-01 JFK.Apr 9, 2001 · N9305N · Doug DC983 · Light System WiringSDR TWAA0010009Frame · crackedDURING CHECK-C MAINT, THE FAIRING SUPPORT FRAME WAS CRACKED AT STA 946, RBL 7 AND LBL 7. REPAIRED BOTH PER SRM 53-05, FIG 81, PAGE 267.Jun 20, 2000 · N9305N · Doug DC983 · Aerodynamic FairingsSDR TWAA0010008Floorbeam · corrodedDURING CHECK-C MAINT, THE FLOORBEAM WAS CORRODED AT STA 1323, LBL 22. REPAIRED FLOORBEAM PER SRM 53-05 PAGE 31 FIG 20A.Jun 16, 2000 · N9305N · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0010503Skin · corrodedDURING CHECK-C MAINT, THE SURFACE AT LE AT TELESCOPING ANTI-ICE DUCT, 0.045 IN MATERIAL WAS REMOVED FOR CORROSION REMOVAL. MATERIAL THICKNESS IS 0.250 IN PER SRM 57-31-1 FIG 1 CORROSION REMOVED ON NR 2-42 BLEND OUT OF CORROSION COMPLIES WITH THE 20 PER CENT Jun 13, 2000 · N9305N · Doug DC983 · Wing, Plate/SkinSDR TWAA0009710Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON FLOORBEAM AT STA 1309, LOCATED 6 INCHES LEFT OF CENTER LINE. REMOVED AND REPLACED FLOOR SUPPORT. USED TWA (P/N 56-2789) TO FABRICATE PER SRM 53-14-3, PAGE 49, AND USED HI-LOKS PER SRM 51-30-5.Jun 13, 2000 · N9305N · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0009708Frame · corrodedDURING CHECK-C MAINT, FOUND FORMER RING AT STA 1309 CORRODED BETWEEN LONGERONS 29L AND 29R. REMOVED CORROSION PER SPM 6-80-01. TRIMMED CORRODED AREA OVER LONGERON AND REPAIRED PER SRM 53-05, FIG 2A.Jun 12, 2000 · N9305N · Doug DC983 · Fuselage Main, FrameSDR TWAA0009611Attach Angle · crackedDURING CHECK-C MAINT, THE ATTACH ANGLE ON BOTTOM OF DORSAL FIN CRACKED THROUGH THE SCREW HOLE, LT SIDE APROX STA 1420. INSTALLED REPAIR ANGLE PER SRM 53-01 PAGE 0 WITH FASTENERS PER SRM 51-10-3.Jun 12, 2000 · N9305N · Doug DC983 · Ventral StructureSDR TWAA0009610Web · corrodedDURING CHECK-C MAINT, THE MEMBRANE AT LONGERON 18L BETWEEN STATION 218 TO 237, O/B OF CHAIR TRACK, WAS CORRODED. FABRICATED NEW PART PER DRAWING 5930544 AND 9930538, AND SRM 51-10-3. INSTALLED PER SRM 51-30 AND 51-10-4.Jun 12, 2000 · N9305N · Doug DC983 · Fuselage Miscellaneous StructureSDR TWAA0009709Structure · damagedDURING CHECK-C MAINT, FOUND CLASS 3 REPAIR AT STA 200 TO 225, LONGERON 4L TO 6L. REPAIRED PER SRM 53-04 FIG 12B, SHEETS 9 AND 10. MESSAGE SENT TO ENGINEERING PER GP&P MANUAL.Jun 11, 2000 · N9305N · Doug DC983 · Fuselage Main, StructureSDR TWAA0009707Seat Track · corrodedDURING CHECK-C MAINT, FOUND INTERGRANULAR CORROSION ON NUMBER 4 CHAIR TRACK, RBL 22 INCHES, STA 1144. INSTALLED SPLICE REPAIR PER SRM 53-05, FIG 4F.Jun 11, 2000 · N9305N · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0009612Attach Angle · crackedDURING CHECK-C MAINT, THE RT DORSAL FIN ATTACH ANGLE ON FUSELAGE STA 1420 WAS CRACKED. INSTALLED NEW ANGLE PER DOUGLAS DRAWING 174968, PER SPM 6-70-01 WITH FASTENERS PER SRM 51-10-3.Jun 11, 2000 · N9305N · Doug DC983 · Fuselage Main, Attach FittingsSDR TWAA0009609Seat Track · corrodedDURING CHECK-C MAINT, CABIN STA 1155 LRL 47 HAD CORROSION ON TRACK NUMBER 2. REPLACED TRACK SECTION PER SRM 53-05, FIG 4F.Jun 8, 2000 · N9305N · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0009608Floorboard · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON CABIN FLOOR PANEL SUPPORT AT STA 200, BL 0 TO RBL 50. REMOVED CORROSION PER SPM 6-80-1. REPLACED SUPPORT EXTRUSION PER DWG 5930545 AND SPM 6-70-01. TREATED PER SRM 51-10-3.Jun 8, 2000 · N9305N · Doug DC983 · Fuselage Floor PanelSDR TWAA0009607Seat Track · corrodedDURING CHECK-C MAINT, NUMBER 3 CHAIR TRACK FROM STA 1031 TO 1309 HAD CORROSION BEYOND LIMITS. REPLACED NUMBER 3 CHAIR TRACK PER IPC 53-40-00 FIG 19B AND SRM 53-05 FIG 4F AND SRM 51-60-0. FIFTEEN FEET 9 INCHES OF TRACK REPLACED WITH TRACK SPLICE AT THE AFT ENJun 8, 2000 · N9305N · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0012105Spar · corrodedDURING CHECK-C MAINT ON THE RT WING, CORROSION WAS FOUND ON THE REAR SPAR BETWEEN CENTER AND O/B AILERON HINGE. FABRICATED ACCORDING TO SRM 59-09 FIG 5. FABRICATED, FINISHED, AND INSTALLED FILLER SHIM AND DOUBLER PER SRM 57-09 FIG 5 AND SRM 57-01 PARAGRAPH 3Jun 7, 2000 · N9305N · Doug DC983 · Wing SparSDR TWAA0009604Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON CABIN FLOORBEAM, LEFT AFT LAV STA 1338, 20 INCH LBL AND 30 IN LBL. CORROSION REMOVED PER SPM 6-80-01 PAGE 31 TO 42, AND SRM 51-10-3 PARAGRAPH 23. REPAIRED DAMAGED AREA PER SSRM 53-00-101 PAGE 201.Jun 7, 2000 · N9305N · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0009606Seat Track · wornDURING CHECK-C MAINT, THE FIRST OFFICER''S RT FWD CHAIR TRACK WAS WORN ON UPPER AND LOWER SURFACES. REPLACED FLOOR TRACK PER MM 53-40-01 PAGE 203.Jun 6, 2000 · N9305N · Doug DC983 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA0009406Frame · corrodedDURING CHECK-C MAINT, THE AFT CARGO BIN HAD CORROSION ON FORMER RING AT STA 1271, LONGERON 30. AT STA 1271 ON FORMER RING AT LONGERON 30 REMOVED CORROSION PER SPM 6-80-01. CUT OUT DAMAGED PORTION OF FORMER RING AND REPAIRED WITH SPLICE PER SRM 53-03, FIG 2A Jun 6, 2000 · N9305N · Doug DC983 · Fuselage Main, FrameSDR TWAA0009405Bracket · crackedDURING CHECK-C MAINT, A FUSELAGE ANGLE BRACKET WAS CRACKED AT STA 946, LBL 7 INSIDE KEEL BEAM LOWER FWD CORNER. FABRICATED PART FROM 7075-T6 PER SPM AND PRINT 9936368, SHEET 1 PART 101.Jun 6, 2000 · N9305N · Doug DC983 · Fuselage Miscellaneous StructureSDR TWAA0009605Stiffener · crackedDURING CHECK-C MAINT AT STA 996 BODY FAIRING STIFFENER BOTTOM CORD HAD A 6.5 INCH CRACK AND THE REPAIR ANGLE HAD 1.5 INCH CRACK. STOP DRILLED CRACKS PER SRM 53-00. ACCOMP NDT HIGH FREQ EDDY CURRENT ON STIFFENER PER 51-00-03 PART 6. FABRICATED NEW ANGLE AND Jun 5, 2000 · N9305N · Doug DC983 · Aerodynamic FairingsSDR TWAA0009304Floor Support · corrodedDURING CHECK-C MAINT AT CABIN STA 1155, LBL 33, FOUND CORROSION ON FLOOR SUPPORT BETWEEN NUMBER 2 AND 3 TRACKS. FABRICATED AND INSTALLED NEW SUPPORT PER SRM 53-14-3, FIG 12 AND SPM 6-70-01 PAGE 3. PROTECTIVE TREATMENT OF SUPPORT PER SRM 51-10-3. INSTALLED WJun 5, 2000 · N9305N · Doug DC983 · Fuselage Miscellaneous StructureSDR TWAA0009005Floorbeam · corrodedDURING CHECK-C MAINT, FOUND CABIN MEMBRANE CORRODED AT STA 503 TO 522, LONGERON 18L. REMOVED CORRODED AREA AND INSTALLED DOUBLER PER SRM 53-01, PAGE 9.Jun 4, 2000 · N9305N · Doug DC983 · Fuselage Main, Floor BeamSDR TWAA0009004Strap · corrodedDURING CHECK-C MAINT, THE RT WING UPPER O/B SPOILER, O/B END, TRAILING EDGE SUPPORT STRAP HAD CORROSION. REMOVED DAMAGED SUPPORT STRAP AND REPLACED WITH NEW PART PER SRM 51-01 ITEM C.Jun 1, 2000 · N9305N · Doug DC983 · SpoilersSDR TWAA9914604Battery · dischargedDURING PREFLIGHT, FOUND OVERHEAD EMERGENCY LIGHTS INOP AT ROWS 28L AND 28R THROUGH ROWS 26L AND R AND 5 EACH INOP IN THE TAIL SECTION. REPLACED BATTERY. AC01 9-14-99 JFK.Oct 28, 1999 · N9305N · Doug DC983 · Emergency LightingSDR TWAA9814305Coalescer Bag · dirtySTRONG ODOR WITH SMOKY HAZE IN COCKPIT AND CABIN AFTER TAKEOFF. FLT RETURNED TO SFO. CHECKED ALL ACFT COMPARTMENTS, CHECKED APU CHECK VALVE, AND ACM OUTLETS FOR OIL. NO SIGN OF OIL. CHANGED BOTH WATER SEPARATORS. ALSO ACCOMP ENG RUN AND PACK BURN OUT PROCSep 6, 1998 · N9305N · Doug DC983 · Humidity Control SystemSDR TWAA9804603Coalescer · dirtyLGA - FLT 293 - AFTER TAKEOFF SMOKE FILLED CABIN AND COCKPIT WITH ODOR AND LIGHT HAZY SMOKE. FLIGHT RETURNED TO LGA. FOUND AIR COND PACK COALESCER BAGS CLOGGED BY DEBRIS FROM BIRD INJESTION. PERFORMED PACK BURNOUT AND REPLACED BOTH COALESCER BAGS. PERFORMEMar 27, 1998 · N9305N · Doug DC983 · Humidity Control SystemSDR TWAA9808816Skin · gougedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND GOUGE IN SKIN PANEL AT LONGERON 22, STATION 1211 TO 1117. REPAIRED SKIN PANEL PER SRM 53-04, FIG 12B. (M)Jun 13, 1997 · N9305N · Doug DC983 · Fuselage Main, Plate/SkinSDR TWAA9806003Skin · gougedMCI - DURING C-CHECK MAINTENANCE FOUND A DEEP GOUGE ON LEFT SIDE OF FUSELAGE, LONGERON 18 TO 26, STATION 1211 TO 1338. REPLACED SKIN PANEL, LONGERON 18 TO 26, STATION 1211 TO 1338, PER SRM 51-10-0, PAGE 1. (M)Jun 13, 1997 · N9305N · Doug DC983 · Fuselage Main, Plate/SkinSDR TWAA9753002Skin · damagedSTL - DURING SPECIAL CHECK, FOUND DAMAGE ON LEFT AFT FUSELAGE, AFT OF FLAP. REPAIRED PER ARA 11135A AND SRM 53-04. (M)Mar 8, 1997 · N9305N · Doug DC983 · Fuselage Main, Plate/SkinSDR 96ZZZM1068Schrader Vlv · failedMSY - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, NOSE LANDING GEAR DID NOT RETRACT. FOLOWED ORH PROCEDURES. FOUND NOSE LANDING GEAR STRUT DEFLATED AND A DEFECTIVE SCHRADER VALVE. SERVICED NOSE LANDING GEAR STRUT WITH HYDRAULIC FLUID AND REPLACED SCHRADEJun 2, 1996 · N9305N · Doug DC983 · Nose/Tail Landing Gear Strut/AxleSDR 96ZZZX3268Coalescer Bag · dirtyMCI - FLT 667 - DURING CLIMB WHEN ENGINE ANTI-ICE WAS TURNED ON, A BURNING ODOR WAS NOTICED IN THE CABIN. TURNED OFF ENGINE ANTI-ICE. FOUND DIRTY COALESCER, MFG PN 21D10-1. REPLACED BOTH COALESCERS. AIR CONDITIONING SYSTEM THEN CHECKED NORMAL. OP-16 - 2-1May 23, 1996 · N9305N · Doug DC983 · Humidity Control System
Back to N9305N, cancelled May 21, 2007