# Service difficulty reports: N938AS, cancelled Mar 21, 2013

A list on [N938AS, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N938AS-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 · 54 reports

- [SDR CALA0001204](https://openairdocs.org/sdr/CALA0001204.md): Actuator · burned · Aug 3, 2000 · N938AS · Doug DC982 · Drag Control Actuator
  > BOTH CREW MEMBERS NOTICED A STRONG ELECTRICAL ODOR IN THE COCKPIT DURING CLIMB OUT OF TPA. CREW WAS UNABLE TO ISOLATE THE SOURCE AND THE AIRCRAFT WAS RETURNED TO TPA WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AUTO SPOILER ACTUATOR IN FORWARD PED
- [SDR CALA0000400](https://openairdocs.org/sdr/CALA0000400.md): Frame · worn · Apr 4, 2000 · N938AS · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A HOLE WORN THROUGH FRAME WEB AT STA 1380, LONGERON 4L. THE FRAME WAS REPAIRED IAW SRM 53-01, FIGURE 4.
- [SDR CALA0000378](https://openairdocs.org/sdr/CALA0000378.md): Pan · corroded · Mar 31, 2000 · N938AS · Doug DC982 · Electrical/Electronic Compartment Doors
  > INSPECTION FOUND E&E DOOR PAN CORRODED BETWEEN THE PAN AND THE E&E DOOR SWITCH AT STA 143, RBL 28. THE CORROSION WAS REMOVED IAW SRM 51-10-03. THE SWITCH BRACKET AND FITTINGS WERE REMOVED IAW SRM 51-30-01 AND 51-30-05. A REPAIR DOUBLER WAS INSTALLED IAW SRM
- [SDR CALA0000377](https://openairdocs.org/sdr/CALA0000377.md): Seat Track · gouged · Mar 31, 2000 · N938AS · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT O/B CABIN SEAT TRACK GOUGED AT STA 1245, LBL 54.5. THE SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-03.
- [SDR CALA0000372](https://openairdocs.org/sdr/CALA0000372.md): Angle · corroded · Mar 30, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT PRESSURE BULKHEAD SIDE LOWER JACK PAD SUPPORT ANGLE CORRODED AT STA 1138, LONGERON 29R. THE JACK PAD HAT ANGLE JACK SUPPORT, STIFFENERS, AND LONGERON FITTINGS WERE REMOVED AND NEW PARTS WERE INSTALLED IAW SRM 51-30-05, 51-30-02.
- [SDR CALA0000363](https://openairdocs.org/sdr/CALA0000363.md): Pan · cracked · Mar 28, 2000 · N938AS · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR FORWARD END INNER PAN CRACKED BY CARGO DOOR LATCHES. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-04, 51-30-05, 51-10-03, AND 52-05, FIGURE 26A.
- [SDR CALA0000362](https://openairdocs.org/sdr/CALA0000362.md): Web · corroded · Mar 28, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT O/B CUSP WEB CORRODED AT FS 1250, LBL 60. THE CORRODED AREAS WERE REMOVED IAW SRM 53-01, FIGURE 4. A DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, FIGURE 4 AND 53-10-03.
- [SDR CALA0000361](https://openairdocs.org/sdr/CALA0000361.md): Strap · cracked · Mar 28, 2000 · N938AS · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND A 1.3 INCH CRACK IN LOWER FORWARD CORNER L-1 DOOR TIE STRAP. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-30-02.
- [SDR CALA0000360](https://openairdocs.org/sdr/CALA0000360.md): Pan · corroded · Mar 28, 2000 · N938AS · Doug DC982 · Passenger/Crew Doors
  > INSPECTION FOUND E & E DOOR PAN CORRODED AROUND AND BETWEEN FWD AND AFT DOOR LOCK FITTINGS AT STA 138 & 148, RBL 28. THE DOOR PAN WAS REPAIRED IAW ECRA 5310-03995.
- [SDR CALA0000359](https://openairdocs.org/sdr/CALA0000359.md): Fitting · cracked · Mar 28, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN FLOOR FITTING AND INTERCOSTAL CORRODED IN FORWARD PIT AT STA 427, L29R. THE FITTING AND INTERCOSTAL WERE REMOVED IAW SRM 51-30-01 AND 51-20-01. A NEW INTERCOSTAL AND FITTING WERE INSTALLED IAW SRM 51-30-02, 51-10-03, AND 51
- [SDR CALA0000358](https://openairdocs.org/sdr/CALA0000358.md): Strap · corroded · Mar 28, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO DOOR LOWER JAMB REPAIR STRAP CORRODED AT FS 1193 - 1212, LONGERON 27R. THE REPAIR STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-30-05, AND ECRA 5310-03027.
- [SDR CALA0000357](https://openairdocs.org/sdr/CALA0000357.md): Fitting · corroded · Mar 28, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR FITTING JUST I/B OF AFT CORNER OF R-1 DOOR, FS 208, RBL 48 CORRODED. THE FLOOR FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-01, 51-10-03, 51-10-04, AND 51-30-02.
- [SDR CALA0000341](https://openairdocs.org/sdr/CALA0000341.md): Angle · cracked · Mar 24, 2000 · N938AS · Doug DC982 · Emergency Exits
  > INSPECTION FOUND LEFT AFT EMERGENCY EXIT DOOR LOWER AFT CORNER SUPPORT ANGLE CRACKED AROUND FASTENER HOLES AND SURFACE CORROSION WAS PRESENT. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-10 AND 51-70-04.
- [SDR CALA0000338](https://openairdocs.org/sdr/CALA0000338.md): Web · cracked · Mar 23, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK AT FASTENER HOLE OF LT O/B CUSP WEB NEAR SEAT TRACK SPLICE FOR LT O/B SEAT TRACK, FS 1220. THE CRACKED AREA OF CUSP WEB WAS REMOVED IAW SRM 53-01. DOUBLER AND FILLER WERE INSTALLED IAW SRM 53-01, 51-10-03, AND 53-01-04.
- [SDR CALA0000337](https://openairdocs.org/sdr/CALA0000337.md): Skin · dented · Mar 23, 2000 · N938AS · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR SKIN DENTED. THE DOOR SKIN WAS REPAIRED IAW SRM 53-04, FIGURE 38 AND 51-30-01.
- [SDR CALA0000336](https://openairdocs.org/sdr/CALA0000336.md): Support Bracket · cracked · Mar 23, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND EXTERNAL FUSELAGE SUPPORT BRACKET CRACKED AT STA 798, LONGERON 20R. THE BRACKET WAS REMOVED AND REPAIR WAS INSTALLED IAW SRM 51-30-01, 51-10-04, 51-10-03, AND 51-30-05.
- [SDR CALA0000335](https://openairdocs.org/sdr/CALA0000335.md): Seat Track · corroded · Mar 23, 2000 · N938AS · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT I/B CABIN SEAT TRACK CORRODED FROM STA 1155 - 1212. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK AND SPLICE WERE INSTALLED IAW SRM 51-30-05 AND 51-30-01.
- [SDR CALA0000334](https://openairdocs.org/sdr/CALA0000334.md): Pan · cracked · Mar 23, 2000 · N938AS · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR AFT END INNER PAN CRACKED AT CARGO DOOR LATCH. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 51-10-04, 51-10-03, 51-30-05, AND 52-05, FIGURE 26A.
- [SDR CALA0000333](https://openairdocs.org/sdr/CALA0000333.md): Fitting · cracked · Mar 23, 2000 · N938AS · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID PIT DOOR INTERIOR FITTING JUST AFT OF FORWARD HINGE CRACKED. THE FITTING WAS REMOVED AND A NEW FITTING WAS INSTALLED IAW SRM 51-30-01, 51-10-04, AND 51-30-12.
- [SDR CALA0000331](https://openairdocs.org/sdr/CALA0000331.md): Frame · corroded · Mar 22, 2000 · N938AS · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND LONGERON FORMER CORRODED IN AFT CARGO BAY AT STA 1041, LONGERON 29L-30. THE LONGERON FORMER WAS REMOVED AND A NEW LONGERON FORMER WAS INSTALLED IAW SRM 51-30-05 AND 51-10-03.
- [SDR CALA0000326](https://openairdocs.org/sdr/CALA0000326.md): Flange · damaged · Mar 20, 2000 · N938AS · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR FORWARD AFT LOWER AND UPPER FLANGES DAMAGED AT STOP POSITION. DOUBLERS WERE INSTALLED IAW SRM 51-30-01, 51-30-02, 51-10-03, AND ECRA 5330-02819.
- [SDR CALA0000325](https://openairdocs.org/sdr/CALA0000325.md): Skin · dented · Mar 20, 2000 · N938AS · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND THREE SHARP DENTS IN MID CARGO DOOR OUTER SKIN. THE DENTED AREA WAS REPAIRED BY INSTALLING DOUBLERS IAW SRM 53-04, FIGURE 38.
- [SDR CALA0000324](https://openairdocs.org/sdr/CALA0000324.md): Skin · bent · Mar 20, 2000 · N938AS · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND AFT CARGO DOOR SKIN AROUND HANDLE BENT AND CHAFED. THE DAMAGED AREA WAS CUT OUT IAW SRM 52-05, FIGURE 3. REPAIR DOUBLERS, FILLER, AND SHIMS WERE INSTALLED IAW SRM 52-05.
- [SDR CALA0000323](https://openairdocs.org/sdr/CALA0000323.md): Floor Support · broken · Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SUB FLOOR MEMBRANE BROKEN AT FS 196, LBL 44 JUST FORWARD OF LT O/B SEAT TRACK. THE SUB FLOOR MEMBRANE WAS REPAIRED IAW SRM 53-01, FIGURE 4 AND 51-30-02.
- [SDR CALA0000322](https://openairdocs.org/sdr/CALA0000322.md): Floor Support · corroded · Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 146 - 200 JUST LEFT OF CENTERLINE. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-01, 51-10-01, AND 51-10-03.
- [SDR CALA0000321](https://openairdocs.org/sdr/CALA0000321.md): Angle · cracked · Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT GILL LINER SUPPORT FRAME CRACKED IN AFT CARGO BAY AT STA 1271. THE SUPPORT ANGLE WAS REMOVED, REPAIRED, AND INSTALLED IAW SRM 51-30-02, 51-10-04, AND 51-30-05.
- [SDR CALA0000319](https://openairdocs.org/sdr/CALA0000319.md): Floor Support · cracked · Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT GILL LINER SUPPORT FRAME CRACKED IN AFT CARGO BAY AT STA 1136. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-02, 51-10-04, AND 51-30-05.
- [SDR CALA0000318](https://openairdocs.org/sdr/CALA0000318.md): Floor Support · cracked · Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO BAY LT UPPER AND LOWER GILL LINER SUPPORT FRAMES CRACKED AT STA 1212. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-30-02 AND 51-30-05.
- [SDR CALA0000317](https://openairdocs.org/sdr/CALA0000317.md): Floor Support · corroded · Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT SIDE FLOOR SUPPORT CORRODED AT STA 180 - 200. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-01, FIGURE 1, 51-10-03, 51-30-02, AND 51-30-05.
- [SDR CALA0000316](https://openairdocs.org/sdr/CALA0000316.md): Seat Track · corroded · Mar 20, 2000 · N938AS · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT O/B CABIN SEAT TRACK CORRODED FROM STA 220 - 237. THE SEAT TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-02, 51-10-04, 51-10-03, AND 51-30-05.
- [SDR CALA0000315](https://openairdocs.org/sdr/CALA0000315.md): Shear Tie · corroded · Mar 20, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SHEAR TIE CORRODED IN AFT CARGO BAY AT STA 1231, LONGERON 29L-30. THE SHEAR TIE WAS REMOVED AND REPLACED IAW SRM 51-30-02.
- [SDR CALA0000313](https://openairdocs.org/sdr/CALA0000313.md): Support · corroded · Mar 18, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND UPPER AND LOWER SURFACES OF FLOOR SUPPORT ANGLE CORRODED IN AFT CARGO BAY AT STA 1117-1155. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-01, 51-10-04, AND 51-10-03.
- [SDR CALA0000312](https://openairdocs.org/sdr/CALA0000312.md): Angle · chafed · Mar 18, 2000 · N938AS · Doug DC982 · Landing Gear Doors
  > INSPECTION FOUND RT MLG DOOR AFT LOWER INNER CORNER REPAIR ANGLE DEEPLY CHAFED. AN INNER CORNER DOUBLER REPAIR WAS INSTALLED IAW SRM 52-05, FIGURE 28, 51-10-04, AND 51-10-03.
- [SDR CALA0000311](https://openairdocs.org/sdr/CALA0000311.md): Stop · worn · Mar 18, 2000 · N938AS · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD CARGO DOOR FORWARD AND AFT LOWER FLANGE AND STOP PADS WORN. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02819.
- [SDR CALA0000310](https://openairdocs.org/sdr/CALA0000310.md): Stop · worn · Mar 18, 2000 · N938AS · Doug DC982 · Cargo/Baggage Doors
  > INSPECTION FOUND MID CARGO DOOR FORWARD AND AFT LOWER FLANGE AND STOP PADS WORN. THE AREAS WERE REPAIRED USING A DOUBLER IAW ECRA 5330-02819 AND SRM 51-10-03.
- [SDR CALA0000309](https://openairdocs.org/sdr/CALA0000309.md): Frame · cracked · Mar 18, 2000 · N938AS · Doug DC982 · Fuselage Main, Frame
  > INSPECTION FOUND A 3 CRACK IN AFT CARGO BAY RT GILL LINER SUPPORT FRAME AT STA 1041, RBL24. THE ANGLE SUPPORT WAS REMOVED AND A NEW ANGLE SUPPORT WAS INSTALLED IAW SRM 51-30-05 AND 51-10-04.
- [SDR CALA0000306](https://openairdocs.org/sdr/CALA0000306.md): Intercostal · corroded · Mar 15, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL CORRODED IN AFT CARGO BAY AT STA 1136-1155, LONGERON 29L. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA0000305](https://openairdocs.org/sdr/CALA0000305.md): Bracket · cracked · Mar 15, 2000 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT FORWARD EMERGENCY EXIT DOOR BINDING DUE TO A CRACKED FORWARD SIDE LT BRACKET. THE CRACK WAS 1.5 INCH LONG AND THE BRACKET WAS LOCATED AT FS 864, LONGERON 13L. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-08 AND 5
- [SDR CALA9901517](https://openairdocs.org/sdr/CALA9901517.md): Strut · deflated · Nov 21, 1999 · N938AS · Doug DC982 · Nose/Tail Landing Gear Strut/Axle
  > THE NOSE GEAR UNSAFE LIGHT REMAINED ON AFTER GEAR RETRACTION DEPARTING DEN AND THE AIRCRAFT WOULD NOT PRESSURIZE UNTIL PULLING THE RIGHT GROUND CONTROL RELAY. THE ABNORMAL CHECKLIST WAS COMPLETED AND THE NOSE GEAR LIGHT EXTINGUISHED. THE AIRCRAFT WAS RETURNE
- [SDR CALA9801916](https://openairdocs.org/sdr/CALA9801916.md): Oven · failed · Oct 7, 1998 · N938AS · Doug DC982 · Buffet/Galleys
  > AN ELECTRICAL BURNING ODOR WAS NOTICED IN THE FORWARD CABIN AREA WHILE EN ROUTE TO ATL. NO VISIBLE SMIKE WAS PRESENT. THE AIRCRAFT LANDED AT ATL WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD GALLEY NR 2 OVEN HAD A BURNED MOTOR. THE OVEN WAS PLACARDED INOP
- [SDR CALA9801497](https://openairdocs.org/sdr/CALA9801497.md): Valve · leaking · Aug 23, 1998 · N938AS · Doug DC982 · Brake Anti-Skid Section
  > THE RT HYDRAULIC SYSTEM QUANTITY DECREASED DURING CLIMBOUT. QRH PROCEDURES WERE FOLLOWED FOR HYDRAULIC QUANTITY LOSS AND ALTERNATE GEAR EXTENSION WAS USED FOR RETURN TO MCO WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT INBOARD ANTI-SKI
- [SDR CALA9800991](https://openairdocs.org/sdr/CALA9800991.md): Prox Sensor · inoperative · Jun 8, 1998 · N938AS · Doug DC982 · Landing Gear Position and Warning
  > THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED. THE FLIGHT WAS CONTINUED TO ORD WHERE IT LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND THE NLG UPLOCK PROXIMITY SENSOR AT FAULT. TH
- [SDR CALA9800412](https://openairdocs.org/sdr/CALA9800412.md): Beam · corroded · Mar 11, 1998 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MID BAGGAGE BIN Z-ANGLE BEAM CORRODED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIGURE 63.
- [SDR CALA9800396](https://openairdocs.org/sdr/CALA9800396.md): Doubler · corroded · Mar 5, 1998 · N938AS · Doug DC982 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND NR 2 RADIO ALT RECEIVER ANTENNA RETAINING DOUBLER CORRODED. THE RETAINING DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-00 AND 51-30-2.
- [SDR CALA9700054](https://openairdocs.org/sdr/CALA9700054.md): Compressor · damaged · Jan 9, 1997 · N938AS · Doug DC982 · Turbine Engine Compressor Section
  > THE AIRCRAFT WAS DIVERTED TO DEN WITH THE NR 1 ENGINE SHUTDOWN WHILE EN ROUTE. THE AIRCRAFT LANDED IN DEN WITHOUT INCIDENT. AN ENGINE CHANGE IS IN PROGRESS. *S/D* INVESTIGATION REVEALED THAT THE ENGINE FAILURE WAS CAUSED BY INGESTION OF BLUE ICE ORIGINATIN
- [SDR ASAA9680208](https://openairdocs.org/sdr/ASAA9680208.md): Evac Slide · broken · Sep 22, 1996 · N938AS · Doug DC982 · Escape Slide
  > SEA - PRIOR TO DEPARTURE OF FLIGHT 598 - CREW REPORTED THE R1 DOOR EMERGENCY EVACUATION SLIDE DEPLOY LANYARD WAS BROKEN AND DETACHED. REPLACED THE EMERGENCY EVACUATION SLIDE. (M)
- [SDR ASAA9680082](https://openairdocs.org/sdr/ASAA9680082.md): Batteries · discharged · Mar 28, 1996 · N938AS · Doug DC982 · Emergency Lighting
  > SEA - DURING MAINTENANCE CHECK, THE EMERGENCY EXIT FLOOR TRACK LIGHTS AT ROWS 13 THROUGH 18 WERE FOUND INOPERATIVE. REPLACED BATTERIES IN POWER SUPPLY AND LIGHT OPERATED NORMALLY. (M)
- [SDR ASAA9680081](https://openairdocs.org/sdr/ASAA9680081.md): Coalescers · contam check · Mar 27, 1996 · N938AS · Doug DC982 · Humidity Control System
  > LAS - FLT NR 9000, AIRCRAFT WAS RELEASED FOR MAINTENANCE FERRY FLIGHT TO SEA (REF MRR ASAA9680080). AFTER TAKEOFF, BOTH PILOTS DETECTED AND ODOR IN THE COCKPIT WHICH MAINTENANCE TECH FOREMAN OCCUPYING THE OBSERVERS SEAT ATTRIBUTED TO A HOT DUCT ODOR. AIRCRAF
- [SDR ASAA9680080](https://openairdocs.org/sdr/ASAA9680080.md): Tr Return Line · leaking · Mar 26, 1996 · N938AS · Doug DC982 · Engine Thrust Reverser
  > LAS - FLT NR 624 - CREW REPORTED AN ELECTRICAL OR HOT PLASTIC ODOR IN THE CABIN DURING DESCENT AND LANDING. INSPECTION OF ALL LAVATORY WASTE CONTAINERS, OVENS, BUN WARMERS AND COFFEE MAKERS REVEALED NO PLASTIC RESIDUE OR OVERHEAT CONDITION, ODOR HAS DISSIPATE
- [SDR 96ZZZM700](https://openairdocs.org/sdr/96ZZZM700.md): Coalescers · dirty · Mar 26, 1996 · N938AS · Doug DC982 · Humidity Control System
  > LAS - FLT NR 624 - CREW REPORTED AN ELECTRICAL OR HOT PLASTIC ODOR IN THE CABIN DURING DESCENT AND LANDING. INSPECTION OF ALL LAVATORY WASTE CONTAINERS, OVENS, BUN WARMERS AND COFFEE MAKERS REVEALED NO PLASTIC RESIDUE OR OVERHEAT CONDITION, ODOR HAS DISSIPATE

Next page: https://openairdocs.org/deregistered/N938AS-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 = 'N938AS' AND deregistration_id = 'N938AS-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N938AS-2013-03-21/reports

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