# Service difficulty reports: N9305N, cancelled May 21, 2007 A list on [N9305N, cancelled May 21, 2007](https://openairdocs.org/deregistered/N9305N-2007-05-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR AALA20040847](https://openairdocs.org/sdr/AALA20040847.md): Connector · shorted · Aug 14, 2004 · N9305N · Doug DC983 · Electrical Connectors > INFLIGHT 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 A - [SDR ZW0A0212902](https://openairdocs.org/sdr/ZW0A0212902.md): Valve · defective · Dec 26, 2002 · N9305N · Doug DC983 · Nose/Tail Landing Gear Strut/Axle > NOSE GEAR STRUT FLAT NOT ALLOWING GEAR TO RETRACT. REMOVED AND REPLACED SCHRADER VALVE AND RESERVICED STRUT. - [SDR ZW0A0212801](https://openairdocs.org/sdr/ZW0A0212801.md): Seal · loose · Dec 23, 2002 · N9305N · Doug DC983 · Cabin Cooling System > BOTH HEAT EXCHANGERS LEAKING NOT ALLOWING AIRCRAFT TO PRESSURIZE. TIGHTENED SEALS ON BOTH HEAT EXCHANGERS. - [SDR ZW0A0210401](https://openairdocs.org/sdr/ZW0A0210401.md): Power Supply · discharged · Oct 8, 2002 · N9305N · Doug DC983 · Emergency Lighting > THE EGRESS LIGHTING BETWEEN ROWS 15 TO 21 WERE FLASHING ON AND OFF DURING FLIGHT. REPLACED THE POWER SUPPLY. - [SDR ZW0A0206201](https://openairdocs.org/sdr/ZW0A0206201.md): Fitting · cracked · Jun 11, 2002 · N9305N · Doug DC983 · Fuselage Miscellaneous Structure > DURING 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. - [SDR ZW0A0206003](https://openairdocs.org/sdr/ZW0A0206003.md): Floorbeam · damaged · Jun 5, 2002 · N9305N · Doug DC983 · Fuselage Main, Floor Beam > DURING 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. - [SDR ZW0A0205902](https://openairdocs.org/sdr/ZW0A0205902.md): Tie Clip · cracked · Jun 4, 2002 · N9305N · Doug DC983 · Fuselage Miscellaneous Structure > DURING CHECK-C CRACKED TIE CLIP AT STA 1437 VERT BULKHEAD TO LONG 3R. REPLACED TIE CLIP PER SPM 6-70-01. - [SDR ZW0A0205303](https://openairdocs.org/sdr/ZW0A0205303.md): Floorbeam · corroded · May 22, 2002 · N9305N · Doug DC983 · Fuselage Main, Floor Beam > DURING 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. - [SDR ZW0A0205302](https://openairdocs.org/sdr/ZW0A0205302.md): Stringer · cracked · May 17, 2002 · N9305N · Doug DC983 · Fuselage Main, Longeron/Stringer > DURING CHECK-C MAINT STRINGER 3 LT WAS CRACKED AT STA 160, ABOVE ELECT PANEL. REPAIRED LONGERON 3 PER SRM 53-02, FIG 18. - [SDR ZW0A0205301](https://openairdocs.org/sdr/ZW0A0205301.md): Door Frame · cracked · May 17, 2002 · N9305N · Doug DC983 · Service Doors > DURING 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. - [SDR ZW0A0205203](https://openairdocs.org/sdr/ZW0A0205203.md): Longeron · cracked · May 16, 2002 · N9305N · Doug DC983 · Fuselage Main, Longeron/Stringer > DURING CHECK-C MAINT THE NUMBER 4 LT LONGERON WAS CRACKED AT STA 160. REPLACED DAMAGED SECTION OF LONGERON PER SRM 53-02, FIG 18. - [SDR ZW0A0111203](https://openairdocs.org/sdr/ZW0A0111203.md): Wire · broken · Nov 25, 2001 · N9305N · Doug DC983 · Light System Wiring > DURING PREFLIGHT INSPECTION IT WAS NOTED THE RH MID ZONE EGRESS LIGHTS WERE INOP. REPAIRED BROKEN WIRE AT ROW 16 RH SIDE. - [SDR ZW0A011123](https://openairdocs.org/sdr/ZW0A011123.md): Wire · broken · Nov 25, 2001 · N9305N · Doug DC983 · Light System Wiring > DURING PREFLIGHT INSPECTION IT WAS NOTED THE RH MID ZONE EGRESS LIGHTS WERE INOP. REPAIRED BROKEN WIRE AT ROW 16 RT SIDE. - [SDR ZW0A0107502](https://openairdocs.org/sdr/ZW0A0107502.md): Battery Pack · Aug 25, 2001 · N9305N · Doug DC983 · Emergency Lighting > THE CABIN OVERHEAD EMERGENCY LIGHTS ILLUMINATED WHEN POWER WAS REMOVED FROM THE AIRCRAFT. REPLACED THE BATTERY PACK. CHECK-C 5-7-01 STL. --CLOSED-- - [SDR ZW0A0107101](https://openairdocs.org/sdr/ZW0A0107101.md): Lamp · Aug 17, 2001 · N9305N · Doug DC983 · Landing Gear Retraction/Extension System > DURING 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 --- - [SDR ZW0A0106303](https://openairdocs.org/sdr/ZW0A0106303.md): Battery Pack · discharged · Aug 4, 2001 · N9305N · Doug DC983 · Emergency Lighting > DURING 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. - [SDR ZW0A0103202](https://openairdocs.org/sdr/ZW0A0103202.md): Battery Pack · discharged · Jun 8, 2001 · N9305N · Doug DC983 · Emergency Lighting > IN FLIGHT THE EGRESS LIGHTS AT ROWS 15 TO 22 ILLUMINATED. REPLACED THE BATTER PACK. CHECK-C 5-7-01 STL. - [SDR ZW0A0102705](https://openairdocs.org/sdr/ZW0A0102705.md): Power Supply · discharged · Jun 2, 2001 · N9305N · Doug DC983 · Emergency Lighting > AN OVERWING EMERGENCY EXIT LIGHT REMAINED ON IN FLIGHT. REPLACED THE POWER SUPPLY. CHECK-C 5-7-01 STL. - [SDR ZW0A0102302](https://openairdocs.org/sdr/ZW0A0102302.md): Battery · discharged · May 24, 2001 · N9305N · Doug DC983 · Emergency Lighting > THE EGRESS LIGHTING IN THE FIRST CLASS CABIN WAS INOPERATIVE. REPLACED THE BATTERIES IN THE BATTERY PACK. CHECK-C 5-7-01 STL. - [SDR TWAA0106301](https://openairdocs.org/sdr/TWAA0106301.md): Wire · broken · Apr 9, 2001 · N9305N · Doug DC983 · Light System Wiring > THE AFT CABIN EXIT IDENTIFIER FAILED TO ILLUMINATE. REPAIRED A BROKEN WIRE IN CEILING OF AFT LEFT LAVATORY. CHECK-C 2-5-01 JFK. - [SDR TWAA0010009](https://openairdocs.org/sdr/TWAA0010009.md): Frame · cracked · Jun 20, 2000 · N9305N · Doug DC983 · Aerodynamic Fairings > DURING 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. - [SDR TWAA0010008](https://openairdocs.org/sdr/TWAA0010008.md): Floorbeam · corroded · Jun 16, 2000 · N9305N · Doug DC983 · Fuselage Main, Floor Beam > DURING CHECK-C MAINT, THE FLOORBEAM WAS CORRODED AT STA 1323, LBL 22. REPAIRED FLOORBEAM PER SRM 53-05 PAGE 31 FIG 20A. - [SDR TWAA0010503](https://openairdocs.org/sdr/TWAA0010503.md): Skin · corroded · Jun 13, 2000 · N9305N · Doug DC983 · Wing, Plate/Skin > DURING 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 - [SDR TWAA0009710](https://openairdocs.org/sdr/TWAA0009710.md): Floorbeam · corroded · Jun 13, 2000 · N9305N · Doug DC983 · Fuselage Main, Floor Beam > DURING 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. - [SDR TWAA0009708](https://openairdocs.org/sdr/TWAA0009708.md): Frame · corroded · Jun 12, 2000 · N9305N · Doug DC983 · Fuselage Main, Frame > DURING 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. - [SDR TWAA0009611](https://openairdocs.org/sdr/TWAA0009611.md): Attach Angle · cracked · Jun 12, 2000 · N9305N · Doug DC983 · Ventral Structure > DURING 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. - [SDR TWAA0009610](https://openairdocs.org/sdr/TWAA0009610.md): Web · corroded · Jun 12, 2000 · N9305N · Doug DC983 · Fuselage Miscellaneous Structure > DURING 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. - [SDR TWAA0009709](https://openairdocs.org/sdr/TWAA0009709.md): Structure · damaged · Jun 11, 2000 · N9305N · Doug DC983 · Fuselage Main, Structure > DURING 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. - [SDR TWAA0009707](https://openairdocs.org/sdr/TWAA0009707.md): Seat Track · corroded · Jun 11, 2000 · N9305N · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings > DURING 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. - [SDR TWAA0009612](https://openairdocs.org/sdr/TWAA0009612.md): Attach Angle · cracked · Jun 11, 2000 · N9305N · Doug DC983 · Fuselage Main, Attach Fittings > DURING 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. - [SDR TWAA0009609](https://openairdocs.org/sdr/TWAA0009609.md): Seat Track · corroded · Jun 8, 2000 · N9305N · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings > DURING CHECK-C MAINT, CABIN STA 1155 LRL 47 HAD CORROSION ON TRACK NUMBER 2. REPLACED TRACK SECTION PER SRM 53-05, FIG 4F. - [SDR TWAA0009608](https://openairdocs.org/sdr/TWAA0009608.md): Floorboard · corroded · Jun 8, 2000 · N9305N · Doug DC983 · Fuselage Floor Panel > DURING 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. - [SDR TWAA0009607](https://openairdocs.org/sdr/TWAA0009607.md): Seat Track · corroded · Jun 8, 2000 · N9305N · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings > DURING 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 EN - [SDR TWAA0012105](https://openairdocs.org/sdr/TWAA0012105.md): Spar · corroded · Jun 7, 2000 · N9305N · Doug DC983 · Wing Spar > DURING 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 3 - [SDR TWAA0009604](https://openairdocs.org/sdr/TWAA0009604.md): Floorbeam · corroded · Jun 7, 2000 · N9305N · Doug DC983 · Fuselage Main, Floor Beam > DURING 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. - [SDR TWAA0009606](https://openairdocs.org/sdr/TWAA0009606.md): Seat Track · worn · Jun 6, 2000 · N9305N · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings > DURING 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. - [SDR TWAA0009406](https://openairdocs.org/sdr/TWAA0009406.md): Frame · corroded · Jun 6, 2000 · N9305N · Doug DC983 · Fuselage Main, Frame > DURING 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 - [SDR TWAA0009405](https://openairdocs.org/sdr/TWAA0009405.md): Bracket · cracked · Jun 6, 2000 · N9305N · Doug DC983 · Fuselage Miscellaneous Structure > DURING 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. - [SDR TWAA0009605](https://openairdocs.org/sdr/TWAA0009605.md): Stiffener · cracked · Jun 5, 2000 · N9305N · Doug DC983 · Aerodynamic Fairings > DURING 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 - [SDR TWAA0009304](https://openairdocs.org/sdr/TWAA0009304.md): Floor Support · corroded · Jun 5, 2000 · N9305N · Doug DC983 · Fuselage Miscellaneous Structure > DURING 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 W - [SDR TWAA0009005](https://openairdocs.org/sdr/TWAA0009005.md): Floorbeam · corroded · Jun 4, 2000 · N9305N · Doug DC983 · Fuselage Main, Floor Beam > DURING 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. - [SDR TWAA0009004](https://openairdocs.org/sdr/TWAA0009004.md): Strap · corroded · Jun 1, 2000 · N9305N · Doug DC983 · Spoilers > DURING 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. - [SDR TWAA9914604](https://openairdocs.org/sdr/TWAA9914604.md): Battery · discharged · Oct 28, 1999 · N9305N · Doug DC983 · Emergency Lighting > DURING 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. - [SDR TWAA9814305](https://openairdocs.org/sdr/TWAA9814305.md): Coalescer Bag · dirty · Sep 6, 1998 · N9305N · Doug DC983 · Humidity Control System > STRONG 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 PROC - [SDR TWAA9804603](https://openairdocs.org/sdr/TWAA9804603.md): Coalescer · dirty · Mar 27, 1998 · N9305N · Doug DC983 · Humidity Control System > LGA - 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. PERFORME - [SDR TWAA9808816](https://openairdocs.org/sdr/TWAA9808816.md): Skin · gouged · Jun 13, 1997 · N9305N · Doug DC983 · Fuselage Main, Plate/Skin > MCI - 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) - [SDR TWAA9806003](https://openairdocs.org/sdr/TWAA9806003.md): Skin · gouged · Jun 13, 1997 · N9305N · Doug DC983 · Fuselage Main, Plate/Skin > MCI - 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) - [SDR TWAA9753002](https://openairdocs.org/sdr/TWAA9753002.md): Skin · damaged · Mar 8, 1997 · N9305N · Doug DC983 · Fuselage Main, Plate/Skin > STL - DURING SPECIAL CHECK, FOUND DAMAGE ON LEFT AFT FUSELAGE, AFT OF FLAP. REPAIRED PER ARA 11135A AND SRM 53-04. (M) - [SDR 96ZZZM1068](https://openairdocs.org/sdr/96ZZZM1068.md): Schrader Vlv · failed · Jun 2, 1996 · N9305N · Doug DC983 · Nose/Tail Landing Gear Strut/Axle > MSY - 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 SCHRADE - [SDR 96ZZZX3268](https://openairdocs.org/sdr/96ZZZX3268.md): Coalescer Bag · dirty · May 23, 1996 · N9305N · Doug DC983 · Humidity Control System > MCI - 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 - 2-1 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N9305N-2007-05-21/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.