# Service difficulty reports: N941AS, cancelled Nov 19, 2012

A list on [N941AS, cancelled Nov 19, 2012](https://openairdocs.org/deregistered/N941AS-2012-11-19.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 · 72 reports

- [SDR AALA20050313](https://openairdocs.org/sdr/AALA20050313.md): Battery Pack · discharged · May 8, 2005 · N941AS · Doug DC982 · Emergency Lighting
  > LGA - SEAT MOUNTED EMERGENCY LIGHTS AFT OF ROW 20 INOPERATIVE. REPLACED CHARGER AND BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AFT OF ROW 20. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20050027](https://openairdocs.org/sdr/AALA20050027.md): Battery Pack · inoperative · Jan 14, 2005 · N941AS · Doug DC982 · Emergency Lighting
  > DFW - EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED EXTERIOR EMERGENCY LIGHT BATTERY PACK AND CHARGER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR AALA20041044](https://openairdocs.org/sdr/AALA20041044.md): Connector · crossed · Oct 13, 2004 · N941AS · Doug DC982 · Emergency Lighting
  > DFW - EMERGENCY ESCAPE PATH LIGHTS AT FORWARD TAIL STAIRS INOPERATIVE. FOUND CONNECTORS CROSS CONNECTED. RECONNECTED CONNECTORS FOR EMERGENCY ESCAPE PATH LIGHTS AT FORWARD TAIL STAIRS. SYSTEM GROUND CHECKED NORMAL OPERATION.
- [SDR ZW0A0304703](https://openairdocs.org/sdr/ZW0A0304703.md): Battery · inoperative · May 7, 2003 · N941AS · Doug DC982 · Emergency Lighting
  > THE CEILING EMERGENCY LIGHTS WERE INOPERATIVE BETWEEN SEAT ROWS 7 TO 11 AND JUST AFT OF ROW 31, AND THE FIRST CLASS EGRESS LIGHTS WERE DIM. REPLACED THE BATTERIES FOR THE BATTERY PACK FOR BOTH OF THE CEILING LIGHTS, AND CLEANED MOISTURE FROM FLOOR TRACK FOR T
- [SDR ZW0A0203101](https://openairdocs.org/sdr/ZW0A0203101.md): Floor Support · corroded · Mar 13, 2002 · N941AS · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION IN FLOOR SUPPORT FLANGES FROM STATION 160 TO 200, RBL 43. INSTALLED NEW FABRICATED SUPPORT AT STA 160 TO 200, PER SPM 6-70-01.
- [SDR ZW0A0202701](https://openairdocs.org/sdr/ZW0A0202701.md): Floor Support · corroded · Mar 5, 2002 · N941AS · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINTENANCE FOUND CORROSION IN LATERAL FLOOR SUPPORT, STATION 181, FROM RBL 9 TO RBL 42. INSTALLED LATERAL SUPPORT AFTER FABRICATION AT STA 181, FROM RBL 9 TO RBL 42, PER SPM 6-70-01.
- [SDR ZW0A0202603](https://openairdocs.org/sdr/ZW0A0202603.md): Floor Support · corroded · Mar 1, 2002 · N941AS · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND FLOOR SUPPORT CORRODED AT STA 195, LBL 14. REMOVED CORROSION ON MEMBRANE PER SRM 53-01, PAGE 6, AND SPM 6-80-01, PAGES 1, 2, AND 3. REMOVED FLOOR SUPPORT AND FABRICATED NEW PER SPM 6-70-01, PAGES 1, 2, AND 3. INSTALLED FLOOR SUPPO
- [SDR ZW0A0202503](https://openairdocs.org/sdr/ZW0A0202503.md): Floor Support · corroded · Feb 28, 2002 · N941AS · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND CORROSION IN LONGITUDINAL FLOOR SUPPORT FROM STA 160 TO 196, LBL 45. REPLACED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-02.
- [SDR ZW0A0202502](https://openairdocs.org/sdr/ZW0A0202502.md): Seat Track · corroded · Feb 27, 2002 · N941AS · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > DURING CHECK-C MAINT CABIN SEAT TRACK HAD CORROSION IN LT FLANGE OF TRACK, LBL 44.5 INCHES, BETWEEN STA 1117 AND 1174. INSTALLED NEW SECTION OF TRACK FROM STA 1108 TO 1222 PER SPM 6-70-01, PAGE 3. SPLICED PER SRM 53-05, FIG 4F.
- [SDR ZW0A0202404](https://openairdocs.org/sdr/ZW0A0202404.md): Support Bracket · cracked · Feb 25, 2002 · N941AS · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT FOUND A SUPPORT BRACKET CRACKED, 8 INCHES BELOW THE FLOOR TRACK AT STA 845, LBL 22 INCHES. REPLACED SUPPORT PER SPM 6-70-01.
- [SDR ZW0A0103101](https://openairdocs.org/sdr/ZW0A0103101.md): Coupling · defective · Jun 5, 2001 · N941AS · Doug DC982 · Air Distribution System
  > WHILE CREW WAS TROUBLESHOOTING A CABIN TEMPERATURE PROBLEM THE CABIN BEGAN TO CLIMB UNCONTROLLABLY. THE CREW INITIATED AN EMERGENCY DESCENT, MANUALLY DROPPED THE OXY MASKS, AND MADE AN UNSCHEDULED LANDING AT JFK. FOUND RT PACK RAM AIR COUPLING TO HEAT EXCHAN
- [SDR TWAA0015404](https://openairdocs.org/sdr/TWAA0015404.md): Light · inoperative · Oct 3, 2000 · N941AS · Doug DC982 · Emergency Lighting
  > THE EMERGENCY EXIT LIGHT ASSEMBLY IN THE TAIL COMPARTMENT WAS HANGING DOWN AT AN ANGLE, AND THE FIRST CLASS EGRESS LIGHTS WERE INOPERATIVE. RE-INSTALLED LIGHT ASSEMBLY IN THE TAIL COMPARTMENT, AND CLEANED MOISTURE AND DEBRIS FROM THE EGRESS LIGHT STRIP CONNEC
- [SDR TWAA0014901](https://openairdocs.org/sdr/TWAA0014901.md): Battery Pack · discharged · Sep 26, 2000 · N941AS · Doug DC982 · Emergency Lighting
  > THE AFT SECTION OF EGRESS LIGHTS AND THE AFT AIRSTAIR EMERGENCY LIGHT WERE INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 2-22-00 STL.
- [SDR TWAA0011102](https://openairdocs.org/sdr/TWAA0011102.md): Blade · failed · Jul 13, 2000 · N941AS · Doug DC982 · Turbine Section
  > THE RT ENGINE FAILED WITH A BANG. CREW ACCOMPLISHED ENGINE SHUT DOWN PROCEDURE AND MADE AN UNSCHEDULED LANDING AT IAD. FOUND TURBINE FAILURE. CHECK-C 2-22-00 STL. EXCESSIVE CROSS NOTCH WEAR OF THIRD STAGE TURBINE BLADES WAS THE ROOT CAUSE OF THE FAILURE.
- [SDR TWAA0010001](https://openairdocs.org/sdr/TWAA0010001.md): Csd · failed · Jun 23, 2000 · N941AS · Doug DC982 · AC Generation System
  > IN CLIMB, THE RT CSD WENT ABOVE RED LINE AFTER 20 MINUTES OF FLIGHT. CREW DISCONNECTED THE CSD. THE APU WAS STARTED BUT IN CRUISE AT FL350 THE APU SHUT ITSELF DOWN. RESTARTED APU AT FL280. FLIGHT RETURNED TO LAS. THE APU OIL WAS SERVICED. CORRECTIONS TO
- [SDR TWAA9902601](https://openairdocs.org/sdr/TWAA9902601.md): Support · broken · Feb 2, 1999 · N941AS · Doug DC982 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND AFT CABIN FLOOR SUPPORT BROKEN AT STA 1300, BL 0 IN, AFT CABIN FLOOR BOARD NUMBER 94. INSTALLED REPAIR ANGLE PER ARA 15736.
- [SDR TWAA9902602](https://openairdocs.org/sdr/TWAA9902602.md): Frame · corroded · Jan 31, 1999 · N941AS · Doug DC982 · Fuselage Main, Frame
  > DURING OP 16 MAINT CHECK, FOUND FUSELAGE FRAME LOWER SECTION AT STA 1322, BL 0, WITH CORROSION ABOVE STRINGER. REMOVED CORROSION PER TWA SPM 6-80-01. REPAIRED PER SRM 53-03, FIG 2A.
- [SDR TWAA9902605](https://openairdocs.org/sdr/TWAA9902605.md): Seat Track · corroded · Jan 28, 1999 · N941AS · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > DURING OP 16 MAINT CHECK, FOUND CORROSION AROUND FASTENER HOLES ON FLOOR TRACK RBL 16, BETWEEN STA 1212 AND 1271. INSTALLED NEW FLOOR TRACK PER STANDARD PROCESSES MANUAL 6-70-01, PAGE 3.
- [SDR TWAA9902604](https://openairdocs.org/sdr/TWAA9902604.md): Intercostal · corroded · Jan 28, 1999 · N941AS · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL BELOW RT FLOOR TRACK AT STA 1308, RBL 16, WAS CORRODED. INSTALLED NEW INTERCOSTAL PER STANDARD PROCESSES MANUAL 6-70-1, PAGE 3.
- [SDR TWAA9902603](https://openairdocs.org/sdr/TWAA9902603.md): Intercostal · corroded · Jan 28, 1999 · N941AS · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL CORRODED BELOW LT FLOOR SUPPORT, BETWEEN STA 1308 AND 1319, LBL 16. INSTALLED NEW INTERCOSTAL PER STANDARD PROCESSES MANAL 6-70-1, PAGE 3.
- [SDR TWAA9901906](https://openairdocs.org/sdr/TWAA9901906.md): Casting · cracked · Jan 27, 1999 · N941AS · Doug DC983 · Entrance Stairs
  > DURING OP 16 MAINT CHECK, THE FWD AIRSTAIRS FORWARD DOOR CASTING WAS CRACKED IN RADIUS APPROXIMATELY 1.5 INCH LONG. REMOVED AND REPLACED CASTING PER STANDARD PROCESSES MANUAL 6-70-01.
- [SDR TWAA9901905](https://openairdocs.org/sdr/TWAA9901905.md): Skin · delaminated · Jan 27, 1999 · N941AS · Doug DC983 · Rudder, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND RUDDER DELAMINATED ON RT SIDE AT AFT SIDE OF CENTER HINGE. REPAIRED PER SRM 51-90-0, PAGE 49, AND 51-70-1A PAGE 21.
- [SDR TWAA9901707](https://openairdocs.org/sdr/TWAA9901707.md): Fitting · corroded · Jan 23, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND FLOOR FITTING CORRODED AT STA 1193 AT CUSP LINE, RT SIDE OF AFT CARGO BIN. REMOVED LIGHT SURFACE CORROSION USING RUBBER BACK SANDING DISC AND ALUMINUM OXIDE DISC, PER SPM 6-80-01. REINSTALLED ORIGINAL BOLTS AND NUTS IN FITTING
- [SDR TWAA9901708](https://openairdocs.org/sdr/TWAA9901708.md): Seat Track · corroded · Jan 22, 1999 · N941AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings
  > DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT STA 1099, 44 IN LBL. REMOVED CORROSION PER TWA SPM 6-80-01. INSTALLED NEW TRACK PER SRM 53-05, FIG 4F.
- [SDR TWAA9901706](https://openairdocs.org/sdr/TWAA9901706.md): Frame · corroded · Jan 21, 1999 · N941AS · Doug DC983 · Fuselage Main, Frame
  > DURING OP 16 MAINT CHECK, FOUND CORROSION AT STA 1219 APPROXIMATELY RBL 4 IN UNDERNEATH UPPER PART OF FORMER RING. REMOVED CORROSION PER SRM 6-80-01, PG 1 TO 3. REINSTALLED FORMER FOOT, AFTER CLEANING CORROSION, PER SPM 6-70-01, PG 3 AND USED AD FASTENERS.
- [SDR TWAA9901705](https://openairdocs.org/sdr/TWAA9901705.md): Floorbeam · corroded · Jan 21, 1999 · N941AS · Doug DC983 · Fuselage Main, Floor Beam
  > DURING OP 16 MAINT CHECK, FOUND FLOORBEAM CAP CORRODED AT STA 1156 BETWEEN TRACK LBL 22 AND LBL 42. FABRICATED NEW PART FROM 7075 T6. INSTALLED PER TWA STD PROCESSES MANUAL 6-70-01.
- [SDR TWAA9901704](https://openairdocs.org/sdr/TWAA9901704.md): Web · corroded · Jan 21, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND IN CABIN, WEB CRACKED AND CORRODED AT STA 1156 UNDER FLOOR. REMOVED CORROSION PER SRM 51-10-3, PARA 31 TO 42. REPAIRED WEB PER 53-01, PG 9 FIG 2 SHEET 3.
- [SDR TWAA9901703](https://openairdocs.org/sdr/TWAA9901703.md): Membrane · cracked · Jan 19, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE REPAIR DOUBLER CRACKED IN 2 PLACES AT STA 1271 TO 1307. REMOVED OLD DOUBLER AND INSTALLED NEW ONE PER SRM 53-05, PG 347 TO 351. USED AD FASTENERS PER SRM 6-30-07 PAGE 1 AND 2.
- [SDR TWAA9901702](https://openairdocs.org/sdr/TWAA9901702.md): Membrane · corroded · Jan 19, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOOR MEMBRANE AT STA 927 TO 946, 58.8 LBL. REMOVED 9 INCH BY 13 IN FLOOR MEMBRANE AND INSTALLED NEW 2024-T3 0.040 DOUBLER EXTENDING TWO FASTENER ROWS BEYOND CUT LINE PER SRM 53-01, FIG H, SHEET 3.
- [SDR TWAA9901605](https://openairdocs.org/sdr/TWAA9901605.md): Angle · corroded · Jan 19, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND AFT CARGO COMPT FLOOR SUPPORT ANGLE ON TOP OF FORMER STA 1212 RBL CORRODED. REMOVED AND REINSTALLED ANGLE PER TWA STD PROCESSES 6-70-01.
- [SDR TWAA9901604](https://openairdocs.org/sdr/TWAA9901604.md): Membrane · corroded · Jan 19, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, THE CABIN FLOOR MEMBRANE WAS CORRODED AT STA 743 RT SIDE. REMOVED CORROSION PER STANDARD PROCEDURES MANUAL 6-80-01. FABRICATED AND INSTALLED DOUBLER PER SPM 6-70-01, PG 1.
- [SDR TWAA9901606](https://openairdocs.org/sdr/TWAA9901606.md): Seat Track · corroded · Jan 18, 1999 · N941AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings
  > DURNG OP 16 MAINT CHECK, FOUND IN CABIN, CORROSION IN CHAIR TRACK AT RBL 44 IN, STA 237, 262 TO 264, AND STA 275. REPLACED TRACK RBL 44 FROM STA 237 TO 275 PER SRM 53-005, PG 10G.
- [SDR TWAA9901602](https://openairdocs.org/sdr/TWAA9901602.md): Angle · cracked · Jan 18, 1999 · N941AS · Doug DC983 · Vertical Stabilizer
  > DURING OP 16 MAINT CHECK, FOUND FUSELAGE TO VERTICAL STABILIZER TIE ANGLE CRACKED APPROX 1.5 INCH LONG AT STA 1426 BETWEEN LONGERON 1L AND 2L, INSIDE LOWER STABILIZER. REPLACED ANGLE PART NR 5912188-35 PER STANDARD PROCESSES MANUAL 6-70-01.
- [SDR TWAA9901309](https://openairdocs.org/sdr/TWAA9901309.md): Structure · corroded · Jan 17, 1999 · N941AS · Doug DC983 · Passenger/Crew Doors
  > DURING OP 16 MAINT CHECK, FOUND IN FWD LT CABIN DOOR WHERE SEAL CONTROL SHAFT PASSES THRU INTERNAL STRUCTURE TO CONNECT WITH SEAL ACTUATING LINK, STRUCTURE HAS CORROSION APPROXIMATELY 17 INCHES FROM LE OF DOOR AND 4 INCHES FROM BOTTOM OF DOOR. INSTALLED NEW S
- [SDR TWAA9901307](https://openairdocs.org/sdr/TWAA9901307.md): Membrane · corroded · Jan 17, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED AT STA 522 TO 541, RT SIDE. REMOVED CORROSION PER STD PROCESSES MANUAL 6-80-1, PARA B PG 1. REPAIRED PER SRM 53-01, PG 18.
- [SDR TWAA9901306](https://openairdocs.org/sdr/TWAA9901306.md): Membrane · corroded · Jan 17, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND SIDEWALL FLOOR MEMBRANE WITH CORROSION BETWEEN LONGERON 655 AND 658. CUT OUT CORRODED AREA, INSTALLED 3 INCH BY 16 INCH 2024T3 0.032 DOUBLER, PER SRM 53-01, PG 18 FIG 4.
- [SDR TWAA9901305](https://openairdocs.org/sdr/TWAA9901305.md): Membrane · damaged · Jan 16, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND HOLE IN MEMBRANE AT STA 199, APPROXIMATELY LBL 16 INCHES. CUT OUT DAMAGE AND INSTALLED DOUBLER PER SRM 53-01, PAGE 18 FIG 4.
- [SDR TWAA9901209](https://openairdocs.org/sdr/TWAA9901209.md): Intercostal · corroded · Jan 15, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL FOOT CORRODED BETWEEN STA 1212 AND 1219, RBL 4 IN. INSTALLED NEW FOOT PER SRM 6-70-0 PG 3 AND USED FASTENERS PER SPM 6-30-01 PAGE 1 AND 2.
- [SDR TWAA9901208](https://openairdocs.org/sdr/TWAA9901208.md): Membrane · corroded · Jan 15, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED STA 465 TO 475 ON LT SIDE. CUT OUT CORRODED SECTION AND INSTALLED TWO ROW REPAIR DOUBLER PER SRM 53-01, PG 18.
- [SDR TWAA9901207](https://openairdocs.org/sdr/TWAA9901207.md): Membrane · corroded · Jan 15, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORRODED AT STA 400 TO 408, LT SIDE. CUT OUT CORRODED SECTION AND INSTALLED TWO ROW REPAIR DOUBLER PER SRM 53-01, PG 18.
- [SDR TWAA9901206](https://openairdocs.org/sdr/TWAA9901206.md): Membrane · cracked · Jan 15, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND I/B EDGE OF MEMBRANE CRACKED BENEATH CHAIR TRACK AT STA 1063, LBL 42 IN. REPAIRED MEMBRANE PER SRM 53-01, PG 9.
- [SDR TWAA9901205](https://openairdocs.org/sdr/TWAA9901205.md): Membrane · corroded · Jan 15, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE WITH CORROSION BETWEEN STA 598 AND 617 AT CABIN SIDEWALL AREA. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLER PER SRM 53-01, FIG 2.
- [SDR TWAA9901204](https://openairdocs.org/sdr/TWAA9901204.md): Membrane · corroded · Jan 14, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND FLOOR MEMBRANE CORROSION AT STA 484 TO 502 ON RT SIDE. REMOVED CORROSION PER SPM 6-80-01. REPAIRED PER SRM 53-01, PG 9.
- [SDR TWAA9901203](https://openairdocs.org/sdr/TWAA9901203.md): Seat Track · corroded · Jan 14, 1999 · N941AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings
  > DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT STA 1206, LBL 22 IN. REPLACED CORRODED SECTION OF CHAIR TRACK PER SRM 53-05, PG 10G.
- [SDR TWAA9901202](https://openairdocs.org/sdr/TWAA9901202.md): Seat Track · corroded · Jan 13, 1999 · N941AS · Doug DC983 · Fuselage, Seat/Cargo Attach Fittings
  > DURING OP 16 MAINT CHECK, FOUND CORROSION IN CHAIR TRACK AT RBL 22 IN STA 237. REMOVED APPROX 60 INCHES OF SEAT TRACK STARTING AT STA 200. INSTALLED NEW TRACK AND SPLICE PER SRM 53-05, FIG 4F.
- [SDR TWAA9901201](https://openairdocs.org/sdr/TWAA9901201.md): Rib · cracked · Jan 12, 1999 · N941AS · Doug DC983 · Wing, Rib/Bulkhead
  > DURING OP 16 MAINT CHECK, FOUND ON RT WING 2 CRACKS ON RIB LOCATED ONE FT O/B OF NR 8 TRACK. STOP DRILLED CRACKS AND INSTALLED DOUBLER PER SRM 57-01, FIG 3 SHEET 3.
- [SDR TWAA9900604](https://openairdocs.org/sdr/TWAA9900604.md): Hanger · cracked · Jan 7, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND LOWER FAIRING T HANGER AT STA 865, 0 IN BL, WAS CRACKED. INSTALLED NEW T HANGER BRACKET (P/N 3936409-505), PER TWA STANDARD PROCEDURES MANUAL 6-70-01.
- [SDR TWAA9900605](https://openairdocs.org/sdr/TWAA9900605.md): Hanger · cracked · Jan 4, 1999 · N941AS · Doug DC983 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, THE LOWER FAIRING T HANGER WAS FOUND CRACKED AT 0 IN BL AND STA 875. INSTALLED NEW BRACKET (P/N 3936409-501) PER TWA STANDARD PROCESSES MANUAL 6-70-01.
- [SDR ASAA9880169](https://openairdocs.org/sdr/ASAA9880169.md): Bottle · discharged · Sep 3, 1998 · N941AS · Doug DC982 · Escape Slide
  > LAX - DURING MAINTENANCE CHECK, THE R1 DOOR EMERGENCY EVACUATION SLIDE INFLATION BOTTLE PRESSURE WAS FOUND LOW. REPLACED THE R1 DOOR EMERGENCY EVACUATION SLIDE ASSY. (M)
- [SDR ASAA9880165](https://openairdocs.org/sdr/ASAA9880165.md): Light · inoperative · Aug 29, 1998 · N941AS · Doug DC982 · Emergency Lighting
  > SEA - DURING MAINTENANCE CHECK, THE FORWARD PORTABLE EMERGENCY LIGHT NEON ARM INDICATOR LIGHT WAS FOUND INOPERATIVE. REPLACED THE LIGHT ASSEMLBY AND OPERATED NORMALLY. (M)

Next page: https://openairdocs.org/deregistered/N941AS-2012-11-19/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 = 'N941AS' AND deregistration_id = 'N941AS-2012-11-19'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N941AS-2012-11-19/reports

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