# Service difficulty reports: N27783, cancelled Apr 24, 2003

A list on [N27783, cancelled Apr 24, 2003](https://openairdocs.org/deregistered/N27783-2003-04-24.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 · 70 reports

- [SDR CALA9900699](https://openairdocs.org/sdr/CALA9900699.md): Skin · corroded · Jun 17, 1999 · N27783 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN BULGED AFT OF EXTERNAL POWER RECEPTACLE AT STA 294, WL 160. THE BULGED AREA WAS CUT OUT. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-30-3.
- [SDR CALA9900693](https://openairdocs.org/sdr/CALA9900693.md): Skin · bulged · Jun 16, 1999 · N27783 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT FUSELAGE BELLY SKIN BULGED AT FS 360 AFT OF MLG. A REPAIR WAS INSTALLED IAW SRM 51-10-1, 51-10-2, AND 51-30-2.
- [SDR CALA9900692](https://openairdocs.org/sdr/CALA9900692.md): Wire · broken · Jun 16, 1999 · N27783 · Boeing 727232 · Light System Wiring
  > INSPECTION FOUND EMERGENCY PATH LIGHTING AT SEAT ROW 28 INOPERATIVE. WIRING WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.
- [SDR CALA9900691](https://openairdocs.org/sdr/CALA9900691.md): Wire · broken · Jun 16, 1999 · N27783 · Boeing 727232 · Light System Wiring
  > INSPECTION FOUND EMERGENCY PATH LIGHTING AT ROW 19 AND 20 INOPERATIVE. BROKEN WIRING WAS REPAIRED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.
- [SDR CALA9900690](https://openairdocs.org/sdr/CALA9900690.md): Battery Pack · discharged · Jun 16, 1999 · N27783 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND THE LT AFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-50-00.
- [SDR CALA9900689](https://openairdocs.org/sdr/CALA9900689.md): Battery Pack · discharged · Jun 16, 1999 · N27783 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND MAIN CABIN EXIT LIGHT AT OVERWING EXIT INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.
- [SDR CALA9900688](https://openairdocs.org/sdr/CALA9900688.md): Battery Pack · discharged · Jun 16, 1999 · N27783 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND LT CENTER OVERWING EMERGENCY EXIT LIGHT FLASHING. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.
- [SDR CALA9900687](https://openairdocs.org/sdr/CALA9900687.md): Battery Pack · discharged · Jun 16, 1999 · N27783 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND THE R-2 DOOR EXIT LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED, RECHARGED, AND REINSTALLED AND OPERATION CHECKED GOOD IAW MM 33-50-01, PAGE 501.
- [SDR CALA9900580](https://openairdocs.org/sdr/CALA9900580.md): Connector · failed · May 27, 1999 · N27783 · Boeing 727232 · Landing Gear Position and Warning
  > THE RT MLG RED UNSAFE LIGHT ILLUMINATED STEADILY AT FIRST, AND THEN FLASHED ON AND OFF INTERMITTENTLY WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE TARGETS, SENSORS, AND WIRING WERE VISUALLY INSPECTED AND CHECKED GOOD.
- [SDR CALA9802079](https://openairdocs.org/sdr/CALA9802079.md): Skin · dented · Nov 18, 1998 · N27783 · Boeing 727232 · Trailing Edge Flaps
  > INSPECTION FOUND LT I/B TE FOREFLAP DENTED AND A 1 X 1 AREA OF DEBONDING JUST OUTBOARD OF NR 3 FLAP TRACK AREA AT LOWER SURFACE. THE LT I/B TE FOREFLAP WAS REMOVED AND REPLACED IAW MM 27-51-1.
- [SDR CALA9802076](https://openairdocs.org/sdr/CALA9802076.md): Cover · cracked · Nov 17, 1998 · N27783 · Boeing 727232 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.25 INCH CRACK IN LT WING UPPER T/E HINGE COVER OF NR 3 SPOILER HINGE. THE T/E HINGE COVER WAS REMOVED AND A NEW T/E HINGE COVER WAS INSTALLED IAW SRM 51-20-1 AND 51-30-2, PARAGRAPH 7.
- [SDR CALA9802075](https://openairdocs.org/sdr/CALA9802075.md): Cover · cracked · Nov 17, 1998 · N27783 · Boeing 727232 · Spoilers
  > INSPECTION FOUND A.1875 AND.125 CRACK IN LT WING UPPER T/E HINGE COVER OF NR 2 SPOILER HINGE. THE T/E HINGE COVER WAS REMOVED AND A NEW T/E HINGE COVER WAS INSTALLED IAW SRM 51-30-2, PARAGRAPH 7.
- [SDR CALA9802074](https://openairdocs.org/sdr/CALA9802074.md): Web · punctured · Nov 17, 1998 · N27783 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A PUNCTURE IN FORWARD CARGO AREA WEB JUST FORWARD OF UPPER AFT DOOR STOP. THE PUNCTURED AREA WAS ROUTED OUT IAW SRM 51-10-1, PAGE 6B. A WEB REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-2, FIGURE 1 AND 51-10-2, PAGE 4.
- [SDR CALA9802073](https://openairdocs.org/sdr/CALA9802073.md): Bracket · cracked · Nov 17, 1998 · N27783 · Boeing 727232 · Leading Edge Slat Actuator
  > INSPECTION FOUND TWO.5 INCH CRACKS IN NR 6 LE FLAP O/B ACTUATOR MOUNT BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-20-1, FIGURE 18.
- [SDR CALA9802072](https://openairdocs.org/sdr/CALA9802072.md): Angle · cracked · Nov 17, 1998 · N27783 · Boeing 727232 · Leading Edge Devices
  > INSPECTION FOUND A.375 INCH CRACK IN LT WING NR 2 SLAT LOWER CHORD ANGLE BELOW TELESCOPING ANTI-ICE DUCT AREA. THE CRACK WAS STOP DRILLED AND A REPAIR ANGLE WAS INSTALLED IAW SRM 51-40-4, PAGE 16.
- [SDR CALA9802071](https://openairdocs.org/sdr/CALA9802071.md): Plate · cracked · Nov 17, 1998 · N27783 · Boeing 727232 · Trailing Edge Flaps
  > INSPECTION FOUND A 1 INCH CRACK IN PLATE AT RT INBOARD MIDFLAP ABOVE AFT END OF NR 5 SPINDLE. THE PLATE WAS REMOVED IAW SRM 51-30-2, PAGE 4. A NEW PLATE WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2, PAGE 1.
- [SDR CALA9802070](https://openairdocs.org/sdr/CALA9802070.md): Skin · cracked · Nov 17, 1998 · N27783 · Boeing 727232 · Leading Edge Devices
  > INSPECTION FOUND TWO 1 INCH CRACKS AT SCREW HOLE TO RIVET HOLES OF NR 2 SLAT UPPER TRAILING EDGE WHERE I/B HOOK MOUNTS. THE FASTENERS WERE REMOVED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-10-2, PAGE 3 AND 57-50-3, PAGES 27-28.
- [SDR CALA9802069](https://openairdocs.org/sdr/CALA9802069.md): Skin · cracked · Nov 17, 1998 · N27783 · Boeing 727232 · Leading Edge Devices
  > INSPECTION FOUND A 4 INCH CRACK IN SKIN AT AFT FACE OF LT WING NR 1 SLAT, INBOARD OF INBOARD TRACK AREA. THE NR 1 LE SLAT WAS REMOVED AND REPLACED IAW MM 27-81-11.
- [SDR CALA9701801](https://openairdocs.org/sdr/CALA9701801.md): Accessory Unit · inoperative · Dec 30, 1997 · N27783 · Boeing 727232 · Landing Gear Position and Warning
  > THE LANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT IAW MM 32-09-121. OPERATION OF THE GEAR CHECKED GOOD.
- [SDR CALA9701436](https://openairdocs.org/sdr/CALA9701436.md): Light · inoperative · Oct 14, 1997 · N27783 · Boeing 727232 · Emergency Lighting
  > AFT AIRSTAIR OVERHEAD EMERGENCY LIGHTS INOP. REPLACED LIGHT ASSEMBLY.
- [SDR CALA9701036](https://openairdocs.org/sdr/CALA9701036.md): Floorbeam · corroded · Jun 16, 1997 · N27783 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 480 FROM RBL 46 TO SIDEWALL. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, FIGURE 3.
- [SDR CALA9700961](https://openairdocs.org/sdr/CALA9700961.md): Support · cracked · Jun 15, 1997 · N27783 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT AT STA 720F, BL 0. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
- [SDR CALA9700960](https://openairdocs.org/sdr/CALA9700960.md): Web · cracked · Jun 13, 1997 · N27783 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.5 INCH CRACK IN WEB BELOW CABIN FLOOR TRACK AREA AT BS 885, RBL 45. THE WEB WAS REMOVED AND A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
- [SDR CALA9700959](https://openairdocs.org/sdr/CALA9700959.md): Floorbeam · corroded · Jun 11, 1997 · N27783 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 277, RBL 12. A REPAIR WAS INSTALLED IAW SRM 51-10-1.
- [SDR CALA9701035](https://openairdocs.org/sdr/CALA9701035.md): Floorbeam · corroded · Jun 7, 1997 · N27783 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 1110 BETWEEN RBL 25 AND RBL 46. THE CORROSION WAS REMOVED. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-8.
- [SDR CALA9701034](https://openairdocs.org/sdr/CALA9701034.md): Floorbeam · corroded · Jun 7, 1997 · N27783 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CORROSION ON UPPER SURFACE OF FLOORBEAM AT STA 344, LBL 30. THE CORRODED SECTION WAS CUT OUT. A BEAM REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8.
- [SDR CALA9700958](https://openairdocs.org/sdr/CALA9700958.md): Floor Track · corroded · Jun 7, 1997 · N27783 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND FLOOR TRACK CORRODED AT BS 400 TO 440, RBL 46. THE FLOOR TRACK WAS REMOVED, A NEW TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5.
- [SDR CALA9700957](https://openairdocs.org/sdr/CALA9700957.md): Floor Track · corroded · Jun 7, 1997 · N27783 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND FLOOR TRACK CORRODED AT STA 1110 RBL 25. THE TRACK WAS REMOVED AND A REPLACEMENT TRACK WAS FABRICATED AND INSTALLED IAW SRM 53-10-5.
- [SDR CALA9700947](https://openairdocs.org/sdr/CALA9700947.md): Skin · cracked · Jun 7, 1997 · N27783 · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN RT SIDE OF VERTICAL STABILIZER INNER COMPARTMENT AT RIB NR 8 AND STRINGER 7. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 55-30-05.
- [SDR CALA9700946](https://openairdocs.org/sdr/CALA9700946.md): Skin · cracked · Jun 7, 1997 · N27783 · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN LT SIDE OF VERTICAL STABILIZER INNER COMPARTMENT AT RIB NR 2 AND STRINGER NR 7. THE CRACKED AREA WAS CUT OUT, A REPAIR WAS INSTALLED IAW SRM 55-30-05.
- [SDR CALA9701039](https://openairdocs.org/sdr/CALA9701039.md): Skin · cracked · Jun 6, 1997 · N27783 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND THREE 1 CRACKS AT LT WHEEL WELL KEEL BEAM SKIN AT FORWARD END OF APU CUTOUT, JUST AFT OF BS 870. THE CRACKED AREA WAS CUT OUT. DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-2 AND ECRA 5310-03522.
- [SDR CALA9701037](https://openairdocs.org/sdr/CALA9701037.md): Stringer · cracked · Jun 6, 1997 · N27783 · Boeing 727232 · Wing, Longeron/Stringer
  > INSPECTION FOUND A 1 INCH CRACK IN MID UPPER AFT LT WING STRINGER AT RIB STATION 629. THE CRACK WAS STOP DRILLED. THE STRINGER WAS REPAIRED IAW BOEING SERVICE BULLETIN 57A159.
- [SDR CALA9700962](https://openairdocs.org/sdr/CALA9700962.md): Stringer · cracked · Jun 6, 1997 · N27783 · Boeing 727232 · Wing, Longeron/Stringer
  > INSPECTION FOUND A 1 INCH CRACK IN RT WING STRINGER JUST FORWARD OF FUEL DUMP LINE AT STA 656.50. A REPAIR WAS FABRICATED AND INSTALLED IAW BOEING SERVICE BULLETIN 727-57A159.
- [SDR CALA9700951](https://openairdocs.org/sdr/CALA9700951.md): Stringer · corroded · Jun 6, 1997 · N27783 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 28R IN FORWARD CARGO COMPARTMENT CORRODED AT STA 720E. THE CORRODED SECTION OF STRINGER WAS CUT OUT, A STRINGER AND SPLICE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-3.
- [SDR CALA9700949](https://openairdocs.org/sdr/CALA9700949.md): Floorbeam · cracked · Jun 6, 1997 · N27783 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A.5 INCH CRACK COMING FROM LIGHTENING HOLE IN FLOORBEAM AT BS 825, LBL 54. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.
- [SDR CALA9700948](https://openairdocs.org/sdr/CALA9700948.md): Floorbeam · cracked · Jun 6, 1997 · N27783 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A.5 AND.3125 INCH CRACK OUT OF LIGHTENING HOLE OF FLOORBEAM AT BS 825, RBL 49. THE CRACK WAS STOP DRILLED, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2.
- [SDR CALA9700956](https://openairdocs.org/sdr/CALA9700956.md): Skin · corroded · Jun 5, 1997 · N27783 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED AT BS 720A BETWEEN STRINGER 27R AND 28R. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.
- [SDR CALA9701032](https://openairdocs.org/sdr/CALA9701032.md): Skin · corroded · Jun 4, 1997 · N27783 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FORWARD CARGO COMPARTMENT SKIN BETWEEN STRINGER 27 AND 28 AT STA 720D CORRODED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.
- [SDR CALA9700963](https://openairdocs.org/sdr/CALA9700963.md): Support · corroded · Jun 4, 1997 · N27783 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 424, RBL 45. A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 53-10-5.
- [SDR CALA9700955](https://openairdocs.org/sdr/CALA9700955.md): Stringer · corroded · Jun 4, 1997 · N27783 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER S28R IN FORWARD CARGO COMPARTMENT CORRODED AT STA 620. THE CORRODED SECTION OF STRINGER WAS CUT OUT, A NEW SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3, FIGURE 1.
- [SDR CALA9700954](https://openairdocs.org/sdr/CALA9700954.md): Clip · cracked · Jun 4, 1997 · N27783 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN S28L TIE CLIP AND A.5 INCH CRACK IN S28R TIE CLIP AT STA 460. REPLACEMENT TIE CLIPS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-30-2, AND 51-10-3.
- [SDR CALA9701038](https://openairdocs.org/sdr/CALA9701038.md): Spar · cracked · Jun 3, 1997 · N27783 · Boeing 727232 · Wing Spar
  > INSPECTION FOUND A.75 INCH CRACK IN RT WING FRONT SPAR UPPER CHORD AT STA 335. THE CRACKED SECTION WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW ECRA 5710-01819 AND SRM 57-10-6.
- [SDR CALA9701033](https://openairdocs.org/sdr/CALA9701033.md): Skin · cracked · Jun 3, 1997 · N27783 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.75 INCH CRACK IN FUSELAGE SKIN AT BOTTOM OF WINDOW POST AREA BETWEEN FIRST OFFICER'S WINDSHIELD AND SLIDING WINDOW. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 8.
- [SDR CALA9701031](https://openairdocs.org/sdr/CALA9701031.md): Skin · dented · Jun 2, 1997 · N27783 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A DENT IN RT FUSELAGE SKIN AT STA 1086 TO 1093 BETWEEN STRINGER 21R AND 22R. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1.
- [SDR CALA9701030](https://openairdocs.org/sdr/CALA9701030.md): Bulkhead · cracked · Jun 2, 1997 · N27783 · Boeing 727232 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 2.5 INCH CRACK IN BULKHEAD AT APU LOAD CONTROL CUTOUT, BS 870. THE CRACK WAS STOP DRILLED AND A DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5310-01544.
- [SDR CALA9700953](https://openairdocs.org/sdr/CALA9700953.md): Skin · cracked · Jun 2, 1997 · N27783 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.1875 INCH CRACK IN FUSELAGE SKIN WITH CORROSION AT LAP SEAM BS 600, STRINGER 26L. THE CORROSION WAS REMOVED AND THE CRACKED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.
- [SDR CALA9700952](https://openairdocs.org/sdr/CALA9700952.md): Skin · cracked · Jun 2, 1997 · N27783 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND.0625 INCH CRACKS AROUND RIVET HEADS OF FUSELAGE SKIN AT LAP SEAM 26L BETWEEN BS 575 TO 588. THE CRACKED AREA OF SKIN WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.
- [SDR CALA9700950](https://openairdocs.org/sdr/CALA9700950.md): Skin · corroded · Jun 2, 1997 · N27783 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN BULGING WITH TWO FASTENERS POPPED AT LEFT LAP SEAM 26L BETWEEN BS 700 TO 715. THE CORRODED AREA WAS CUT OUT, A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.
- [SDR CALA9700672](https://openairdocs.org/sdr/CALA9700672.md): Lg Accy Unit · inoperative · May 9, 1997 · N27783 · Boeing 727232 · Landing Gear Position and Warning
  > THE RT MLG RED UNSAFE LIGHT REMAINED ILLUMINATED WHEN LANDING GEAR WAS EXTENDED ON APPROACH. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR ACCESSORY UNIT AND OPERA
- [SDR CALA9601703](https://openairdocs.org/sdr/CALA9601703.md): Duct · broken · Nov 24, 1996 · N27783 · Boeing 727232 · Air Intake Anti/De-Ice System
  > THE NR 3 FIRE LIGHT AND BELL ACTIVATED IN FLIGHT. THE ENGINE THROTTLE WAS REDUCED TO IDLE AND THE WARNING CEASED. WHEN THE THROTTLE WAS INCREASED THE LIGHT CAME ON AGAIN. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND

Next page: https://openairdocs.org/deregistered/N27783-2003-04-24/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 = 'N27783' AND deregistration_id = 'N27783-2003-04-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N27783-2003-04-24/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.