# Service difficulty reports: N37882, cancelled Aug 15, 2003

A list on [N37882, cancelled Aug 15, 2003](https://openairdocs.org/deregistered/N37882-2003-08-15.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 CALA0100582](https://openairdocs.org/sdr/CALA0100582.md): Strut · deflated · Jun 23, 2001 · N37882 · Doug DC981 · Nose/Tail Landing Gear Strut/Axle
  > THE NOSE GEAR UNSAFE LIGHT ILLUMINATED WHILE ENROUTE TO EWR. THE CREW FOLLOWED QRH PROCEDURES. WHEN THE GEAR WAS LOWERED ALL THREE GEAR INDICATED DOWN AND LOCKED. QRH PROCEDURES WERE CONTINUED AND WHEN CREW ATTEMPTED TO RAISE GEAR THE HANDLE WOULD NOT COME UP.
- [SDR CALA0100030](https://openairdocs.org/sdr/CALA0100030.md): Strut · discharged · Jan 16, 2001 · N37882 · Doug DC981 · Nose/Tail Landing Gear Strut/Axle
  > THE NLG WOULD NOT RETRACT AFTER TAKEOFF FROM BOS. THE AIRCRAFT WAS RETURNED TO BOS WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE SWUNG THE NOSE GEAR SEVERAL TIMES AND WAS UNABLE TO DUPLICATE THE FAILURE. THE STRUT PRESSURE WAS FOUND LOW. THE NOSE STRUT WAS
- [SDR CALA0001808](https://openairdocs.org/sdr/CALA0001808.md): Strut · discharged · Nov 18, 2000 · N37882 · Doug DC981 · Nose/Tail Landing Gear Strut/Axle
  > THE NLG WOULD NOT RETRACT AFTER TAKEOFF FROM DTW. THE NOSE GEAR INDICATED UNSAFE AND A LOUD MECHANICAL CLUNKING NOISE WAS HEARD. THE GEAR WAS CYCLED WITH NO CHANGE IN RESULTS. THE GROUND CONTROL ALSO REVERTED TO THE GROUND MODE. THE AIRCRAFT WAS DIVERTED T
- [SDR CALA0001173](https://openairdocs.org/sdr/CALA0001173.md): O-Ring · leaking · Jul 28, 2000 · N37882 · Doug DC981 · Nose/Tail Landing Gear Strut/Axle
  > THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF FROM TPA. QRH PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT WAS DIVERTED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NLG SCHRADER VALVE O-RING LEAKING AND THE STRUT WAS FLAT. THE O-RING WA
- [SDR CALA0000277](https://openairdocs.org/sdr/CALA0000277.md): Support · cracked · Mar 7, 2000 · N37882 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 6 INCH CRACK IN FORWARD CARGO BAY GILL LINER SUPPORT FRAME AT FS 408, LONGERON 25L. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-10-4.
- [SDR CALA0000276](https://openairdocs.org/sdr/CALA0000276.md): Support · corroded · Mar 7, 2000 · N37882 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO LOWER AFT DOOR JAMB CORNER SUPPORT CORRODED AT LONGERON 27R. THE CORNER SUPPORT WAS REMOVED AND A NEW CORNER SUPPORT WAS INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-5.
- [SDR CALA0000269](https://openairdocs.org/sdr/CALA0000269.md): Skin · gouged · Mar 4, 2000 · N37882 · Doug DC981 · Vertical Stabilizer, Plate/Skin
  > INSPECTION FOUND LEFT VERTICAL STABILIZER SKIN GOUGED ALONG HORIZONTAL STABILIZER RUN LINE. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-1, 51-30-2, 51-10-4, AND 51-30-5.
- [SDR CALA0000268](https://openairdocs.org/sdr/CALA0000268.md): Skin · cracked · Mar 4, 2000 · N37882 · Doug DC981 · Service Doors
  > INSPECTION FOUND A CRACK IN FORWARD LAV SERVICE DOOR LOWER AFT CORNER. THE DOOR WAS REMOVED AND A NEW DOOR WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0000267](https://openairdocs.org/sdr/CALA0000267.md): Door Pan · punctured · Mar 4, 2000 · N37882 · Doug DC981 · Service Doors
  > INSPECTION FOUND A PUNCTURE IN R-1 DOOR AT LOWER AFT INTERNAL PAN. A PLUG REPAIR WAS INSTALLED IAW SRM 52-01, FIGURE 1.
- [SDR CALA0000266](https://openairdocs.org/sdr/CALA0000266.md): Angle · cracked · Mar 4, 2000 · N37882 · Doug DC981 · Auxiliary Power Unit (APU) Doors
  > INSPECTION FOUND A 3.5 INCH CRACK IN RT APU DOOR Z-ANGLE AT FS 1320, LONGERON 27R. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-02, 51-10-04, AND 51-10-3.
- [SDR CALA0000265](https://openairdocs.org/sdr/CALA0000265.md): Skin · cracked · Mar 4, 2000 · N37882 · Doug DC981 · Auxiliary Power Unit (APU) Doors
  > INSPECTION FOUND A 2.5 INCH CRACK IN LEFT APU DOOR SKIN AT I/B EDGE, FS 1320, LONGERON 30. THE CRACK WAS STOP DRILLED AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 52-01, FIGURE 2 AND 51-30-2..
- [SDR CALA0000264](https://openairdocs.org/sdr/CALA0000264.md): Angle · cracked · Mar 4, 2000 · N37882 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 4.2 INCH CRACK IN ANGLE IN AFT PIT AT FS 1250-1271, LONGERON 25L. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 53-01, 51-30-1, AND 53-14-3.
- [SDR CALA0000263](https://openairdocs.org/sdr/CALA0000263.md): Angle · cracked · Mar 4, 2000 · N37882 · Doug DC981 · Passenger/Crew Doors
  > INSPECTION FOUND L-1 DOOR UPPER AND LOWER ATTACH ANGLES CRACKED. THE CRACKS WERE 0.75 LONG. THE ANGLES WERE REMOVED AND NEW ANGLES WERE INSTALLED IAW SRM 51-10-3, 51-10-4, 51-30-2, 51-30-5, AND 51-30-7.
- [SDR CALA0000262](https://openairdocs.org/sdr/CALA0000262.md): Frame · cracked · Mar 4, 2000 · N37882 · Doug DC981 · Fuselage Main, Frame
  > INSPECTION FOUND A 2 INCH CRACK IN AFT CARGO BAY GILL LINER SUPPORT FRAME AT STA 1309, LONGERON 23L. THE CRACK WAS STOP DRILLED IAW SRM 53-01-2. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01-2.
- [SDR CALA0000261](https://openairdocs.org/sdr/CALA0000261.md): Floorbeam · cracked · Mar 4, 2000 · N37882 · Doug DC981 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO BAY GILL-LINER FLOOR SUPPORT FRAME AT STA 503, LONGERON 25L. A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA0000260](https://openairdocs.org/sdr/CALA0000260.md): Support · cracked · Mar 4, 2000 · N37882 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MID CARGO BAY BULKHEAD VERTICAL SUPPORT CRACKED AT STA 541. THE VERTICAL SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.
- [SDR CALA0000259](https://openairdocs.org/sdr/CALA0000259.md): Angle · cracked · Mar 4, 2000 · N37882 · Doug DC981 · Horizontal Stabilizer Structure
  > INSPECTION FOUND A 10 INCH CRACK IN HORIZONTAL STABILIZER RIGHT I/B LEADING EDGE I/B ANGLE AT XHR 9.652. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-02, 51-30-05, 51-10-04, AND 51-30-01.
- [SDR CALA0000240](https://openairdocs.org/sdr/CALA0000240.md): Angle · cracked · Mar 3, 2000 · N37882 · Doug DC981 · Engine Cowling System
  > INSPECTION FOUND ANGLE CRACKED THROUGH LOWER ACCESS PANEL NR 7406 OF NR 2 ENGINE NOSE COWL. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-4, 51-10-3, 51-30-5, AND 51-30-2.
- [SDR CALA0000237](https://openairdocs.org/sdr/CALA0000237.md): Skin · cracked · Mar 2, 2000 · N37882 · Doug DC981 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING LEADING EDGE SKIN CRACKED AT I/B END OF REFUELING DOOR. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW SRM 57-06B, FIGURE 3 AND 51-30-1.
- [SDR CALA0000236](https://openairdocs.org/sdr/CALA0000236.md): Frame · cracked · Mar 2, 2000 · N37882 · Doug DC981 · Fuselage Main, Frame
  > INSPECTION FOUND LT SIDE OF CANTED FRAME CRACKED JUST O/B OF LIGHT ASSEMBLY IN TAIL COMPARTMENT AT FS 1485. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-01, FIGURE 2, SHEETS 3 AND 4, 51-30-2, AND 51-30-5, PAGE 4.
- [SDR CALA0000235](https://openairdocs.org/sdr/CALA0000235.md): Beam · corroded · Mar 2, 2000 · N37882 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO DOOR JAMB BEAM CORRODED. THE DOOR JAMB BEAM WAS REPAIRED IAW ECRA 5310-03027, SRM 51-30-2, AND 51-30-5.
- [SDR CALA0000234](https://openairdocs.org/sdr/CALA0000234.md): Fitting · cracked · Mar 2, 2000 · N37882 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LONGERON 25R END FITTING CRACKED IN AFT CARGO BAY AT STA 1220. THE FITTING WAS REMOVED AND NEW FITTING WAS INSTALLED IAW SRM 51-30-5, 51-10-4, AND 51-10-3.
- [SDR CALA0000233](https://openairdocs.org/sdr/CALA0000233.md): Floorbeam · cracked · Mar 2, 2000 · N37882 · Doug DC981 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOOR SUPPORT CRACKED IN AFT CARGO BAY AT STA 1271, L28L. THE FLOOR SUPPORT WAS REMOVED IAW SRM 51-30-2 AND 51-10-4. REMOVED GUSSETS AND FASTENERS FROM INTERCOSTAL TO GAIN ACCESS TO TRAPPED FASTENER AND REINSTALLED IAW SRM 51-30-2 AND 51-10-
- [SDR CALA0000228](https://openairdocs.org/sdr/CALA0000228.md): Skin · dented · Mar 1, 2000 · N37882 · Doug DC981 · Wing, Plate/Skin
  > INSPECTION FOUND RT WING L/E SKIN DENTED JUST FORWARD OF REFUELING DOOR. A REPAIR DOUBLER AND FILLER WERE INSTALLED IAW SRM 57-06B, FIGURE 5, 51-10-4, 51-10-3, 51-20-00, 51-30-2, AND 51-30-5.
- [SDR CALA0000227](https://openairdocs.org/sdr/CALA0000227.md): Frame · cracked · Mar 1, 2000 · N37882 · Doug DC981 · Fuselage Main, Frame
  > INSPECTION FOUND FLOOR SUPPORT FRAMES CRACKED IN AFT CARGO BAY AT STA 1250, L29L AND AT STA 1117, L27L. THE SUPPORTS WERE REMOVED AND NEW SUPPORTS WERE INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-5.
- [SDR CALA0000226](https://openairdocs.org/sdr/CALA0000226.md): Frame · cracked · Mar 1, 2000 · N37882 · Doug DC981 · Fuselage Main, Frame
  > INSPECTION FOUND GILL-LINER SUPPORT FRAMES CRACKED IN AFT CARGO BAY AT STA 1060-1297, L24R TO L27R. THE SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-4 AND 51-30-2.
- [SDR CALA9900443](https://openairdocs.org/sdr/CALA9900443.md): Actuator · leaking · Apr 26, 1999 · N37882 · Doug DC981 · Landing Gear Actuator
  > WITH APU AIR ON AND PACKS ON, CABIN FILLS WITH SMOKE AND STRONG BURNING SMELL. FOUND LEFT GEAR RETRACT ACTUATOR IN TRANSIT LEAK. REMOVED AND REPLACED ACTUATOR PER MM 32-32-02. PERFORMED BURN OUT OF PNEUMATIC DUCT PER MM 21-20-02.
- [SDR CALA990022](https://openairdocs.org/sdr/CALA990022.md): Recepticle · worn · Jan 14, 1999 · N37882 · Doug DC981 · Aerodynamic Fairings
  > TAIL CONE TOP FIVE ALIGNMENT PIN RECEPTICLES WORN. REPLACED TOP FIVE ALIGNMENT PIN RECEPTICLES.
- [SDR CALA9900023](https://openairdocs.org/sdr/CALA9900023.md): Support · corroded · Jan 14, 1999 · N37882 · Doug DC981 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT HAT SECTION CORRODED STA 148 - 200. FABRICATED AND INSTALLED NEW HAT SECTION PER SRM 51-30-01.
- [SDR CALA9800278](https://openairdocs.org/sdr/CALA9800278.md): Longeron · cracked · Feb 20, 1998 · N37882 · Doug DC981 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A.4375 INCH CRACK T CAP AT STA 1338, LONGERON 14R. REPAIRED IAW EA 5310-01272.
- [SDR CALA9800277](https://openairdocs.org/sdr/CALA9800277.md): Pan · cracked · Feb 19, 1998 · N37882 · Doug DC981 · Passenger/Crew Doors
  > INSPECTION FOUND A 1.5 CRACK IN AFT ENTRY DOOR PAN AND A 1.5 CRACK IN INNER PAN ANGLE AT CENTER RT DOOR STOP PAD. REPAIRS WERE INSTALLED IAW ECRA 5220-01034.
- [SDR CALA9800275](https://openairdocs.org/sdr/CALA9800275.md): Frame · gouged · Feb 19, 1998 · N37882 · Doug DC981 · Fuselage Main, Frame
  > INSPECTION FOUND THAT THE LEFT HEAT VALVE HAD GOUGED THE FRAME INNER CAP AT STA 1380. A REPAIR STRAP WAS INSTALLED IAW ECRA 5311-01042.
- [SDR CALA9800274](https://openairdocs.org/sdr/CALA9800274.md): Skin · chafed · Feb 19, 1998 · N37882 · Doug DC981 · Cargo/Baggage Doors
  > INSPECTION FOUND FORWARD BAGGAGE BIN LOWER DOOR SKIN CHAFED IN SEVERAL PLACES BELOW LOCK HANDLE. A REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5230-01397.
- [SDR CALA9800273](https://openairdocs.org/sdr/CALA9800273.md): Skin · oversize holes · Feb 18, 1998 · N37882 · Doug DC981 · Vertical Stabilizer
  > INSPECTION FOUND OVERSIZED HOLES IN FUSELAGE SKIN AT OUTER DORSAL FIN ATTACH ANGLE ON LEFT AND RIGHT SIDES. REPAIRED IAW ECRA 5340-01312.
- [SDR CALA9800272](https://openairdocs.org/sdr/CALA9800272.md): Cusp Beam · corroded · Feb 17, 1998 · N37882 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP BEAM CORRODED AT STA 200, LONGERON 18L. REPAIRED IAW ECRA 5310-03678.
- [SDR CALA9800271](https://openairdocs.org/sdr/CALA9800271.md): Cusp Beam · corroded · Feb 17, 1998 · N37882 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CUSP BEAM CORRODED AT STA 229, LONGERON 18L. REPAIRED IAW ECRA 5310-03678.
- [SDR CALA9800266](https://openairdocs.org/sdr/CALA9800266.md): Beltframe · corroded · Feb 16, 1998 · N37882 · Doug DC981 · Fuselage Main, Frame
  > INSPECTION FOUND BELTFRAME CORRODED ACROSS BOTTOM ON FRONT CENTER AND LOWER CHANNEL AT STA 1322 FROM LONGERON 28L TO 28R. A REPAIR WAS INSTALLED IAW SRM 53-03.
- [SDR CALA9800257](https://openairdocs.org/sdr/CALA9800257.md): Skin · dented · Feb 16, 1998 · N37882 · Doug DC981 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT FLOOR LEVEL AFT OF L-1 DOOR, STA 218 TO 256, LONGERON 18L. THE SKIN WAS REPAIRED IAW ECRA 5330-01204.
- [SDR CALA9800256](https://openairdocs.org/sdr/CALA9800256.md): Angle · cracked · Feb 13, 1998 · N37882 · Doug DC981 · Passenger/Crew Doors
  > INSPECTION FOUND A.125 INCH CRACK IN MAIN CABIN DOOR ANGLE AT BAYONET CUTOUT. REPAIRED IAW SRM 52-05, FIGURE 33.
- [SDR CALA9800255](https://openairdocs.org/sdr/CALA9800255.md): Beam · cracked · Feb 13, 1998 · N37882 · Doug DC981 · Passenger/Crew Doors
  > INSPECTION FOUND A 1.25 INCH CRACK AT AFT END OF MAIN CABIN DOOR NR 7 BEAM AND A 1 INCH CRACK WAS LOCATED AT FORWARD END OF NR 7 BEAM. A 1 INCH CRACK WAS FOUND AT FORWARD END OF MAIN CABIN DOOR NR 8 BEAM. A.75 INCH CRACK WAS FOUND AT FORWARD END OF MAIN CAB
- [SDR CALA9800217](https://openairdocs.org/sdr/CALA9800217.md): Longeron · corroded · Feb 12, 1998 · N37882 · Doug DC981 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 29R CORRODED UNDER FLANGE AT STA 1322. THE CORRODED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.
- [SDR CALA9800214](https://openairdocs.org/sdr/CALA9800214.md): Pivot Plates · corroded · Feb 10, 1998 · N37882 · Doug DC981 · Horizontal Stabilizer Structure
  > INSPECTION FOUND INBOARD AND OUTBOARD SET OF HINGE PIVOT PLATES CORRODED ON RT HORIZONTAL STABILIZER. THE OUTBOARD SET OF HINGE PIVOT PLATES WERE FOUND CORRODED ON LT HORIZONTAL STABILIZER. THE PIVOT PLATES WERE REMOVED AND REPLACED IAW SRM 51-30-5.
- [SDR CALA9800194](https://openairdocs.org/sdr/CALA9800194.md): Beam · corroded · Feb 5, 1998 · N37882 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND MID BAGGAGE BIN DOOR JAMB BEAM CORRODED. THE AREA WAS REPAIRED IAW SRM 53-05, FIGURE 63.
- [SDR CALA9800150](https://openairdocs.org/sdr/CALA9800150.md): Support · corroded · Jan 30, 1998 · N37882 · Doug DC981 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED BETWEEN PANEL D AND E AT STA 148 TO 160, FORWARD ENTRY AREA. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 53-01, 51-10-3, AND 51-30-2.
- [SDR CALA9700179](https://openairdocs.org/sdr/CALA9700179.md): Actuator · leaking · Feb 14, 1997 · N37882 · Doug DC981 · Trailing Edge Flap Actuator
  > THE RT HYDRAULIC SYSTEM QUANTITY INDICATED ZERO ACCOMPANIED BY THE RT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATING WHILE EN ROUTE. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT INBOARD FLAP ACTUATOR LEAKING. THE FLAP ACTUATOR WAS REPLACED IAW
- [SDR CALA9601817](https://openairdocs.org/sdr/CALA9601817.md): Actuator · leaking · Dec 11, 1996 · N37882 · Doug DC981 · Trailing Edge Flap Actuator
  > THE RT HYDRAULIC QUANTITY WAS LOST WHILE ON APPROACH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SEAL LEAKING AT LEFT INBOARD FLAP ACTUATOR. THE LT INBOARD FLAP ACTUATOR CYLINDER WAS REPLACED IAW MM 27-52-02. THE FLAPS AND ALL OTHER FLIGHT CON
- [SDR CALA9601055](https://openairdocs.org/sdr/CALA9601055.md): Bus Gen Cont · inoperative · Jul 25, 1996 · N37882 · Doug DC981 · AC Power Distribution System
  > BOTH GENERATOR OFF-LIGHTS ILLUMINATED AND ALL GENERATOR POWER WAS LOST DURING CLIMB AT 9,000 FEET. THE AC CROSSTIE LOCKOUT LIGHT ALSO CAME ON. THE GENERATORS WERE RESET AND OPERATION WAS NORMAL, BUT THE AC CROSSTIE LOCKOUT LIGHT REMAINED ILLUMINATED. THE FL
- [SDR CALA9600871](https://openairdocs.org/sdr/CALA9600871.md): Ckt Breaker · failed · Jun 25, 1996 · N37882 · Doug DC981 · AC Power Distribution System
  > THE RT AC BUS 50 AMP CIRCUIT BREAKER, AFT CENTER AND LEFT FUEL BOOST PUMP CIRCUIT BREAKERS POPPED WHILE EN ROUTE. CREW ATTEMPTED TO RESET CIRCUIT BREAKERS WITHOUT SUCCESS. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND
- [SDR CAL960424](https://openairdocs.org/sdr/CAL960424.md): Strut · flat · Mar 29, 1996 · N37882 · Doug DC981 · Nose/Tail Landing Gear Strut/Axle
  > FLT NR 303 - EWR - THE N/G WOULD NOT RETRACT AFTER T/O FROM EWR. THE GEAR HANDLE WAS CYCLED SEVERAL TIMES, BUT WOULD NOT RAISE BEYOND HALFWAY POINT. THE AUTO SPOILER 'DO NOT' USE LIGHT WAS ON AND THE A/C WOULD NOT PRESSURIZE. THE A/C WAS RETURNED TO EWR WHE
- [SDR CAL960109](https://openairdocs.org/sdr/CAL960109.md): Handle · lack of lube · Feb 8, 1996 · N37882 · Doug DC981 · Trailing Edge Flap Control System
  > FLT NR 1490 - CLE - THE FLAP/SLAT HANDLE WOULD NOT LOCK INTO THE SLAT RETRACT POSITION. WHEN HOLDING FLAP/SLAT HANDLE TO SLAT RETRACT POSITION THE SLAT DISAGREE LIGHT CAME ON AND BOTH LEFT AND RIGHT HYDRAULIC GAUGES DROPPED. THE DIAL-A-FLAP WAS MOVED SEVERAL

Next page: https://openairdocs.org/deregistered/N37882-2003-08-15/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 = 'N37882' AND deregistration_id = 'N37882-2003-08-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N37882-2003-08-15/reports

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