# Service difficulty reports: N936AS, cancelled Mar 21, 2013 A list on [N936AS, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N936AS-2013-03-21.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 58 reports - [SDR CALA0000129](https://openairdocs.org/sdr/CALA0000129.md): Skin · cracked · Feb 2, 2000 · N936AS · Doug DC982 · Wing, Plate/Skin > INSPECTION FOUND A 2 INCH CRACK IN RT WING FIXED LEADING EDGE SKIN AT SLAT TRACK NR 8 CUTOUT. THE SKIN WAS REPAIRED IAW ECRA 5721-01049. - [SDR CALA0000107](https://openairdocs.org/sdr/CALA0000107.md): Floorbeam · cracked · Jan 28, 2000 · N936AS · Doug DC982 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOOR SUPPORT CRACKED AT FS 1098, L24L, IN AFT CARGO PIT. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-70-01 AND 51-30-02. - [SDR CALA0000106](https://openairdocs.org/sdr/CALA0000106.md): Rib · cracked · Jan 28, 2000 · N936AS · Doug DC982 · Trailing Edge Flaps > INSPECTION FOUND LT WING O/B NR 1 FLAP L/E INTERIOR RIB CRACKED AT FASTENER HOLES. THE RIB WAS REMOVED AND A NEW RIB WAS INSTALLED IAW SRM 57-50-14 AND 51-30-02. - [SDR CALA0000093](https://openairdocs.org/sdr/CALA0000093.md): Frame · cracked · Jan 27, 2000 · N936AS · Doug DC982 · Fuselage Main, Frame > INSPECTION FOUND A 2 INCH CRACK IN TAIL COMPARTMENT FRAME JUST ABOVE THE WATER SEPARATORS AT STA 1418, LONGERON 2R. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-04, 53-01, FIGURE 2, AND 51-30-05. - [SDR CALA0000092](https://openairdocs.org/sdr/CALA0000092.md): Angle · cracked · Jan 27, 2000 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 3 INCH CRACK IN APU SHROUD CUTOUT AREA FORWARD RIGHT SUPPORT ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-10-04, AND 51-10-03. - [SDR CALA0000091](https://openairdocs.org/sdr/CALA0000091.md): Bracket · cracked · Jan 27, 2000 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1.5 CRACK IN LOWER FUSELAGE LT FILLET PANEL SUPPORT BRACKET AT FS 875, S19L. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-05. - [SDR CALA0000086](https://openairdocs.org/sdr/CALA0000086.md): Angle · cracked · Jan 26, 2000 · N936AS · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND ANGLE CRACKED AT FORWARD CARGO DOOR UPPER SIDE JUST FORWARD OF AFT HINGE. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-02. - [SDR CALA0000078](https://openairdocs.org/sdr/CALA0000078.md): Angle · cracked · Jan 24, 2000 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD FACE OF LAV BULKHEAD FRAME TO FUSELAGE ATTACH ANGLE CRACKED AT STA 1309. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 29. - [SDR CALA0000077](https://openairdocs.org/sdr/CALA0000077.md): Intercostal · cracked · Jan 24, 2000 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND INTERCOSTAL CRACKED IN CABIN UNDER CENTER FLOORBOARD AT FS 769-807. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-05 AND 51-30-02. - [SDR CALA0000076](https://openairdocs.org/sdr/CALA0000076.md): Seat Track · corroded · Jan 24, 2000 · N936AS · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LT O/B SEAT TRACK CORRODED AT STA 1155. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 51-30-2, 53-05, FIGURE 4F, 51-10-4, 51-10-3, AND 51-30-05. - [SDR CALA0000057](https://openairdocs.org/sdr/CALA0000057.md): Frame · corroded · Jan 21, 2000 · N936AS · Doug DC982 · Fuselage Main, Frame > INSPECTION FOUND FRAME IN TAIL COMPARTMENT CORRODED AT FS 1401, S21R. THE FRAME WAS REMOVED AND A NEW FRAME WAS INSTALLED IAW SRM 51-30-21 AND 51-30-05. - [SDR CALA0000056](https://openairdocs.org/sdr/CALA0000056.md): Bulkhead · cracked · Jan 21, 2000 · N936AS · Doug DC982 · Fuselage Main, Bulkhead > INSPECTION FOUND A CRACK IN BULKHEAD AT STA 1309 BETWEEN LONGERONS 15R AND 16R. THE CRACK WAS STOP DRILLED IAW SRM 53-14-03, FIGURE3 AND A REPAIR WAS INSTALLED IAW SRM 51-10-04, 51-10-03, AND 51-30-05. - [SDR CALA0000040](https://openairdocs.org/sdr/CALA0000040.md): Seat Track · corroded · Jan 18, 2000 · N936AS · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RT I/B SEAT TRACK CORRODED FROM STA 200-237. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1 AND 51-30-5. - [SDR CALA0000039](https://openairdocs.org/sdr/CALA0000039.md): Angle · corroded · Jan 18, 2000 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND LOWER AND TOP SURFACES OF ATTACH ANGLE CORRODED AND GOUGED AT FORWARD ENTRY DOOR JAMB LOWER THRESHOLD. THE ATTACH ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 53-11-1, AND 51-30-5. - [SDR CALA0000038](https://openairdocs.org/sdr/CALA0000038.md): Seat Track · corroded · Jan 18, 2000 · N936AS · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LT I/B SEAT TRACK CORRODED AT STA 1079-1193. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-5 AND 51-10-4. - [SDR CALA0000037](https://openairdocs.org/sdr/CALA0000037.md): Angle · corroded · Jan 18, 2000 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND THE R-1 DOOR SLIDE ATTACH ANGLE CORRODED. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-1, 51-10-4, AND 51-10-3. - [SDR CALA0000036](https://openairdocs.org/sdr/CALA0000036.md): Web · corroded · Jan 18, 2000 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR WEB CORRODED INSIDE CABIN ATSTA 1140 JUST INSIDE L-2 DOOR. THE CORROSION WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-01, FIGURE 2 AND 51-10-3. - [SDR CALA0000034](https://openairdocs.org/sdr/CALA0000034.md): Skin · cracked · Jan 18, 2000 · N936AS · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND A.5 INCH CRACK IN BOTH THE LT AND RT MLG DOOR CUTOUTS AT STA 946, LBL 8 AND RBL 8, RESPECTIVELY. THE CRACKED AREAS WERE REMOVED AND ANGLE REPAIRS WERE INSTALLED IAW SRM 53-01, FIGURE 2, 51-10-2, 51-80-5, 53-14-0, FIGURE 2, 51-10-3, AND 51-30 - [SDR CALA9801856](https://openairdocs.org/sdr/CALA9801856.md): Link · broken · Sep 23, 1998 · N936AS · Doug DC982 · Landing Gear Retraction/Extension System > THE RT MLG LIGHT AND GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION LEAVING MIA. THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED SAFELY. MAINTENANCE FOUND THE RT MLG UP ACTUATOR LOWER LINK BROKEN. THE LINK WAS REMOVED AND REPLACED IAW MM 3 - [SDR CALA9800144](https://openairdocs.org/sdr/CALA9800144.md): Air Distribution · smoke · Jan 31, 1998 · N936AS · Doug DC982 · Air Distribution System > THE FLIGHT ATTENDANTS REPORTED HAZE IN CABIN WHILE ON DESCENT. BOTH PACKS WERE RUN ON AIR CART WITH CABIN AND PACKS CHECKING GOOD. THE APU WAS RUN ALL NIGHT WITH PACKS ON. NO SMOKE IN CABIN OR LEAKS AT APU WERE NOTED. - [SDR CALA9800098](https://openairdocs.org/sdr/CALA9800098.md): Cable · damaged · Jan 21, 1998 · N936AS · Doug DC982 · Aerodynamic Fairings > INSPECTION FOUND TAILCONE RELEASE CABLE KINKED AT TOP LEFT PULLEY. THE CABLE WAS REMOVED AND REPLACED AND RIGGED IAW MM 53-53-00. - [SDR CALA9800014](https://openairdocs.org/sdr/CALA9800014.md): Bracket · cracked · Jan 10, 1998 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND BRACKET ANGLE CRACKED IN MID BAG BIN ABOVE LT OUTBOARD FORWARD CORNER OF FUEL TANK. A NEW BRACKET WAS INSTALLED IAW SRM 51-30-5. - [SDR CALA9800013](https://openairdocs.org/sdr/CALA9800013.md): Cables · out of adjust · Jan 10, 1998 · N936AS · Doug DC982 · Aerodynamic Fairings > PULL FROM THE TAIL CONE INTERIOR RELEASE HANDLE WAS EXCESSIVE AT 40 POUNDS. THE LATCH CABLES WERE RIGGED IAW MM 53-53-00. - [SDR CALA9800009](https://openairdocs.org/sdr/CALA9800009.md): Jamb · corroded · Jan 7, 1998 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND Z-ANGLE BEAM REPAIR STRAP CORRODED AT AFT CARGO BIN LOWER DOOR JAMB. THE REPAIR STRAP WAS REPLACED IAW SRM 53-05, FIGURE 63. - [SDR CALA9701396](https://openairdocs.org/sdr/CALA9701396.md): Batteries · discharged · Sep 29, 1997 · N936AS · Doug DC982 · Emergency Lighting > INSPECTION FOUND EMERGENCY OVERHEAD LIGHTS AT L-1 AND R-1 DOORS INOPERATIVE. THE POWER SUPPLY BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD. - [SDR ASAA9680196](https://openairdocs.org/sdr/ASAA9680196.md): Batteries · discharged · Sep 8, 1996 · N936AS · Doug DC982 · Emergency Lighting > SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS IN THE AFT CABIN WERE FOUND INOPERATIVE. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M) - [SDR ASAA9680120](https://openairdocs.org/sdr/ASAA9680120.md): Batteries · discharged · May 22, 1996 · N936AS · Doug DC982 · Emergency Lighting > SFO - DURING MAINTENANCE CHECK, THE EMERGENCY FLOOR TRACK LIGHT IN THE FORWARD CABIN WERE FOUND DIM. REPLACED THE BATTERIES AND OPERATED NORMALLY. (M) - [SDR ASAA9680104](https://openairdocs.org/sdr/ASAA9680104.md): Light · defective · Apr 23, 1996 · N936AS · Doug DC982 · Emergency Lighting > PDX - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT WAS FOUND DIM. REPLACED THE LIGHT ASSEMBLY AND OPERATED NORMALLY. (X) - [SDR ASAA9680100](https://openairdocs.org/sdr/ASAA9680100.md): Door Mechanism · out of adjust · Apr 16, 1996 · N936AS · Doug DC982 · Passenger/Crew Doors > SEA - FLT 191 - PRIOR TO DEPARTURE, CREW REPORTED THE L1 DOOR HANDLE WOULD NOT REMAIN IN THE LOCKED POSITION AND THE DOOR WARNING LIGHT WOULD NOT EXTINGUISH. RERIGGED THE L1 DOOR MECHANISM PER MM AND OPERATED NORMALLY. (X) - [SDR ASAA9680078](https://openairdocs.org/sdr/ASAA9680078.md): Downlock Sensor · defective · Mar 24, 1996 · N936AS · Doug DC982 · Landing Gear Position and Warning > SEA - FLT 467 - CREW REPORTED THE NOSE LANDING GEAR LIGHT REMAINED ILLUMINATED AFTER TAKEOFF OAK. FOLLOWED ABNORMAL GEAR INDICATION CHECKLIST, RECYCLED LANDING GEAR AND INDICATION SYSTEM OPERATED NORMALLY. LANDED IN SEA WITHOUT INCIDENT. REPLACED NOSE LANDI - [SDR ASAA9680074](https://openairdocs.org/sdr/ASAA9680074.md): Floor Covering · excess material · Mar 12, 1996 · N936AS · Doug DC982 · Passenger Compartment Equipment > SEA - FLT 511 - AFTER ARRIVAL, CREW REPORTED R1 DOOR HANDLE WAS DIFFICULT TO MOVE. FOUND GIRT BAR FITTING CONTACTING BOTTOM OF DOOR. REMOVED PORTION OF FORWARD GALLEY FLOOR COVERING MATERIAL, REINSTALLED GIRT BAR, AND RESEALED FLOOR. DOOR AND GIRT BAR OPERA - [SDR ASAA9680035](https://openairdocs.org/sdr/ASAA9680035.md): Battery Pack · discharged · Jan 24, 1996 · N936AS · Doug DC982 · Emergency Lighting > SEA - DURING MAINTENANCE CHECK, THE OVERHEAD EMERGENCY LIGHTS FROM ROWS 2 TO 6 WERE FOUND INOPERATIVE. REPLACED THE BATTERY PACK AND OPERATED NORMALLY. (M) - [SDR ASAA9680034](https://openairdocs.org/sdr/ASAA9680034.md): Mechanism · out of adjust · Jan 23, 1996 · N936AS · Doug DC982 · Passenger/Crew Doors > SEA - PRIOR TO DEPARTURE OF FLIGHT 370, CREW REPORTED THE L1 DOOR WOULD NOT CLOSE AND LOCK NORMALLY. ADJUSTED DOOR MECHANISM PER MAINTENANCE MANUAL AND OPERATED NORMALLY. (M) - [SDR ASAA9680033](https://openairdocs.org/sdr/ASAA9680033.md): Seal · rubbing · Jan 21, 1996 · N936AS · Doug DC982 · Passenger/Crew Doors > SEA - DURING MAINTENANCE CHECK, THE R1 DOOR WAS FOUND DIFFICULT TO OPEN. REMOVED EXCESS INTERIOR TRIM SEAL FROM FORWARD UPPER CORNER OF FRAME AND OPERATED NORMALLY. (M) - [SDR ASAA9680032](https://openairdocs.org/sdr/ASAA9680032.md): Door · out of adjust · Jan 21, 1996 · N936AS · Doug DC982 · Passenger/Crew Doors > SEA - DURING MAINTENANCE CHECK, THE L1 DOOR GUST LOCK WAS FOUND INOPERATIVE. RERIGGED DOOR PER MAINTENANCE MANUAL AND OPERATED NORMALLY. (M) - [SDR ASAA9680031](https://openairdocs.org/sdr/ASAA9680031.md): Door Frame · corroded · Jan 20, 1996 · N936AS · Doug DC982 · Cargo/Baggage Doors > PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT DOOR FRAME PAN AT Y370 TO Y427, X-15 TO X-18, Z-18. REPLACED DOOR FRAME PAN IAW DC-9 SRM 51-30-02, AND 53-05. (M) - [SDR ASAA9680030](https://openairdocs.org/sdr/ASAA9680030.md): Cusp · corroded · Jan 20, 1996 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > PAE - DURING 30K CHECK, CORROSION WAS FOUND ON CUSP AT Y200, X-56, Z-0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-03, 51-30-05 AND 53-05. (M) - [SDR ASAA9680029](https://openairdocs.org/sdr/ASAA9680029.md): Intercostal · corroded · Jan 20, 1996 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > PAE - DURING 30K CHECK, CORROSION WAS FOUND ON INTERCOSTAL FROM Y1307 TO Y1322. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-02 AND 51-30-05. (M) - [SDR ASAA9680028](https://openairdocs.org/sdr/ASAA9680028.md): Longeron · corroded · Jan 20, 1996 · N936AS · Doug DC982 · Fuselage Main, Longeron/Stringer > PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 29R FROM Y1117 TO Y1136. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW ASA EA 5310-01396. (M) - [SDR ASAA9680027](https://openairdocs.org/sdr/ASAA9680027.md): Longeron · corroded · Jan 20, 1996 · N936AS · Doug DC982 · Fuselage Main, Longeron/Stringer > PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 30 FROM Y1245 TO Y1271, X-0, Z-50. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-02, 53-14-03 AND 53-02. (M) - [SDR ASAA9680026](https://openairdocs.org/sdr/ASAA9680026.md): Frame · corroded · Jan 20, 1996 · N936AS · Doug DC982 · Fuselage Main, Frame > PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FRAME AT Y1271, Z-50, LONGERON 26L TO 27R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-02 AND 53-03. (M) - [SDR ASAA9680021](https://openairdocs.org/sdr/ASAA9680021.md): Support · cracked · Jan 15, 1996 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > PAE - DURING 30K CHECK, CRACK WAS FOUND ON FLOOR SUPPORT AT Y1287 TO Y1307, X0, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-10-03, 51-30-02 AND 53-14-03. (M) - [SDR ASAA9680020](https://openairdocs.org/sdr/ASAA9680020.md): Support · corroded · Jan 15, 1996 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > PAE - DURING 30K CHECK, CORROSION WAS FOUND ON FLOOR SUPPORT AT Y169 TO Y174, X MINUS 52, Z PLUS 1. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-02, 53-10-01 AND 53-01. (M) - [SDR ASAA9680019](https://openairdocs.org/sdr/ASAA9680019.md): Seat Track · corroded · Jan 15, 1996 · N936AS · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y232 TO Y239, X MINUS 44, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 53-05. (M) - [SDR ASAA9680018](https://openairdocs.org/sdr/ASAA9680018.md): Seat Track · corroded · Jan 15, 1996 · N936AS · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > PAE - DURING 30K CHECK, CORROSION WAS FOUND ON SEAT TRACK AT Y1174, X PLUS 22, Z0. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-01 AND 53-05. (M) - [SDR ASAA9680017](https://openairdocs.org/sdr/ASAA9680017.md): Splice · corroded · Jan 15, 1996 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 28L SPLICE AT Y598. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-05 AND 53-01. (M) - [SDR ASAA9680016](https://openairdocs.org/sdr/ASAA9680016.md): Longeron · corroded · Jan 15, 1996 · N936AS · Doug DC982 · Fuselage Main, Longeron/Stringer > PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 30L AT Y769 TO Y788. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM 51-30-05. (M) - [SDR ASAA9680015](https://openairdocs.org/sdr/ASAA9680015.md): Longeron · corroded · Jan 15, 1996 · N936AS · Doug DC982 · Fuselage Main, Longeron/Stringer > PAE - DURING 30K CHECK, CORROSION WAS FOUND ON LONGERON 29L AT Y210 TO Y236. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC9-SRM 51-10-03, 51-30-02 AND 53-14-01. (M) - [SDR ASAA9680169](https://openairdocs.org/sdr/ASAA9680169.md): Threshold · corroded · Jan 5, 1996 · N936AS · Doug DC982 · Fuselage Miscellaneous Structure > PAE - DURING 30K CHECK, FOUND CORROSION WAS FOUND ON THE UPPER SURFACE OF THE LOWER FLANGE ON THE AFT CARGO COMPARTMENT DOOR THRESHOLD BEAM AT Y1155, LONGERON 28R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5310-01395. (M) - [SDR ASAA9680168](https://openairdocs.org/sdr/ASAA9680168.md): Skin · corroded · Jan 3, 1996 · N936AS · Doug DC982 · Fuselage Main, Plate/Skin > PAE - DURING 30K CHECK, FOUND CORROSION ON THE FUSELAGE SKIN AND INTERNAL DOUBLER AT Y712 TO Y731, LONGERON 28L TO 28R. REMOVED DAMAGED AREA AND INSTALLED NEW PIECES IAW DC-9 SRM AND ASA EA 5330-01223. (M) Next page: https://openairdocs.org/deregistered/N936AS-2013-03-21/reports.md?page=2 ## 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 = 'N936AS' AND deregistration_id = 'N936AS-2013-03-21' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N936AS-2013-03-21/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.