# Service difficulty reports: N283WA, cancelled Nov 7, 2006

A list on [N283WA, cancelled Nov 7, 2006](https://openairdocs.org/deregistered/N283WA-2006-11-07.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 · 51 reports

- [SDR DL72E020609](https://openairdocs.org/sdr/DL72E020609.md): Spar · cracked · May 30, 2002 · N283WA · Boeing 727247 · Wing Spar
  > INSPECTION OF THE CENTER WING REAR SPAR WEB PER AD 2000-14- 07 AND BAC S/B 727-57A0182 REVEALED A.25 INCH CRACK IN THE WEB BELOW THE UPPER SPAR CAP. THE CRACK WAS ROUTED OUT OF THE WEB WITH A 2 INCH CUTOUT AND REPAIRED WITH AN ALUMINUM REPAIR DOUBLER PER ER
- [SDR DL72E011852](https://openairdocs.org/sdr/DL72E011852.md): Coupler · failed · Nov 24, 2001 · N283WA · Boeing 727247 · Autopilot System
  > AFTER TAKEOFF A/C BEGAN TO FISHTAIL. NO YAW DAMPER FLAGS IN VIEW. NO MOVEMENT OF INDICES ON YD INSTRUMENT. RETURN TO AIRPORT FOR LANDING. FOUND LOWER YAW DAMPER FLAG IN VIEW. WILL NOT RETRACT. REPLD YAW DAMP COUPLER. ALSO FOUND LOWER RUDDER POSITION SENSOR SHO
- [SDR DL72E010484](https://openairdocs.org/sdr/DL72E010484.md): Actuator · jammed · Mar 24, 2001 · N283WA · Boeing 727247 · Leading Edge Slat Actuator
  > AFTER TAKEOFF NR 3 KRUEGER FLAP DID NOT RETRACT. REPLACED KRUEGER FLAP ACTUATOR AND SHUTTLE VALVE LEAK AND OPS CHECK OK PER OPN 7054.RII
- [SDR DL72E010320](https://openairdocs.org/sdr/DL72E010320.md): Angle · cracked · Feb 22, 2001 · N283WA · Boeing 727247 · Leading Edge Devices
  > A.25 INCH CRACK AT FWD SIDE OF NR 6 L/E FLAP ACTUATOR MOUNT BOX O/B TRUNNION UPPER ATTACH ANGLE. REPAIRED PER MM.
- [SDR DL72E010319](https://openairdocs.org/sdr/DL72E010319.md): Stiffener · cracked · Feb 22, 2001 · N283WA · Boeing 727247 · Leading Edge Devices
  > FWD SPAR STIFFENER CRACKED AT I/B SIDE OF NR 6 SLAT O/B TRACK. REPLACED STIFFENER PER MM 57-20-021-8.
- [SDR DL72E010318](https://openairdocs.org/sdr/DL72E010318.md): Stiffener · cracked · Feb 22, 2001 · N283WA · Boeing 727247 · Leading Edge Devices
  > FWD SPAR VERTICAL STIFFENER CRACKED AT I/B SIDE OF NR 6 SLAT I/B TRACK. REPLACED STIFFENER PER MM 57-20-021-8.
- [SDR DL72E010269](https://openairdocs.org/sdr/DL72E010269.md): Skin · cracked · Feb 13, 2001 · N283WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN AROUND THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE LOWER HINGE CUTOUT. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 380012-14, REV A.
- [SDR DL72E002176](https://openairdocs.org/sdr/DL72E002176.md): Skin · cracked · Nov 3, 2000 · N283WA · Boeing 727247 · Passenger/Crew Doors
  > THE UPPER HINGE CUTOUT OF THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE SKIN. HFEC INSPECTION OF ADJACENT FASTENER HOLES REVEALED A CRACK INDICATION IN THE BEAR STRAP. THE SKIN CRACK WAS ROUTED OUT AND THE FASTENER HOLE OVERSIZED TO REMOVE ALL CRACKS. TH
- [SDR DL72E002161](https://openairdocs.org/sdr/DL72E002161.md): Light · inoperative · Nov 3, 2000 · N283WA · Boeing 727247 · Flight Compartment Lighting
  > COCKPIT EMERGENCY LIGHT WILL NOT TEST. FOUND LIGHT ASSY TO HAVE BAD ARM ON SWITCH. REPLACED LIGHT ASSY, P/N ON 334701743, S/N ON 2995, S/N OFF 2955.
- [SDR DL72E002121](https://openairdocs.org/sdr/DL72E002121.md): Frame · cracked · Oct 26, 2000 · N283WA · Boeing 727247 · Fuselage Main, Frame
  > THE LT OVERWING EMERGENCY EXIT FRAME AT FS 783.95 WAS FOUND CRACKED. THE CRACKING IS TYPICAL OF BAC S/B 727-53-0197 AND AD 98-11-03. THE CRACKED FRAME WAS REPAIRED AND MODIFIED PER THE S/B AND DOCUMENTED PER ER/A 379029-14AD.
- [SDR DL72E002124](https://openairdocs.org/sdr/DL72E002124.md): Skin · corroded · Oct 25, 2000 · N283WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION AT FS 685 AT STRINGER 27L. THE CORROSION WAS REMOVED WITH A 4 X 5 INCH CUTOUT. THE CUTOUT WAS BETWEEN AN EXISTING DOUBLER REPAIR AT STRINGER 26L AND ANOTHER AT STRINGER 28L. THE EXISTING REPAIRS WERE REM
- [SDR DL72E002144](https://openairdocs.org/sdr/DL72E002144.md): Stiffener · cracked · Oct 17, 2000 · N283WA · Boeing 727247 · Wing Miscellaneous Structure
  > FOUND DURING MV4 CORROSION VISIT NRC 22, L/E SPAR STIFFENER CRACK APPROX 1 INCH AT NR 7 SLAT INBOARD TRACK INBOARD ANGLE. REPLACED ANGLE PER M/M 57-20-21.
- [SDR DL72E002120](https://openairdocs.org/sdr/DL72E002120.md): Angle · corroded · Oct 17, 2000 · N283WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > CORROSION AT STA 740 LWR CHORD (SKIN ATTACH ANGLE) AT AFT END OF STR 27R. REPLACED RT SKIN SUPPORT ANGLE PER 727 M/M 53-11-0 PG 858.
- [SDR DL72E002074](https://openairdocs.org/sdr/DL72E002074.md): Web · cracked · Oct 17, 2000 · N283WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > TWO CRACKS ON RT TORQUE BOX I/B VERT WEB AT UPPER END AT STA 1235. REPAIRED PER MM 53-11-0 PG 832.
- [SDR DL72E001363](https://openairdocs.org/sdr/DL72E001363.md): Angle · cracked · Jul 19, 2000 · N283WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND AT D2 LTR CHECK N/R 42,.5 INCH CRACK EXTENDING BEYOND THE RADIUS BLOCK, TORQUE BOX HORIZONTAL ANGLE FWD SIDE STA 1263. REPLACED ANGLE PER DRD 53-10-10D FIG 803D.
- [SDR DL72E001189](https://openairdocs.org/sdr/DL72E001189.md): Bulkhead · punctured · Jun 18, 2000 · N283WA · Boeing 727247 · Fuselage Main, Bulkhead
  > THE FS 178 BULKHEAD WEB WAS PUNCTURED DUE TO GROUND CONTACT WITH THE WING-TIP OF ANOTHER AIRCRAFT. THE WEB DAMAGED WAS CLEANED UP WITH A 13 X 9 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN ALUMINUM DOUBLER INSTALLED PER ER/A 377552-14, REV A.
- [SDR DL72E001188](https://openairdocs.org/sdr/DL72E001188.md): Beam · cracked · Jun 17, 2000 · N283WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > THE FS 178 BULKHEAD WAS DAMAGED FROM GROUND CONTACT WITH THE WING-TIP OF ANOTHER AIRCRAFT. THE FWD CHORD OF THE LBL 5.7 BEAM WAS SEVERED NEAR WL 180 AND BEAM WEB TORN AT THE SAME LOCATION. THE CHORD WAS CUT TO REMOVE THE DAMAGE AND WEB WAS TRIMMED TO REMOVE
- [SDR DL72E000535](https://openairdocs.org/sdr/DL72E000535.md): Indicator · malfunctioned · Mar 19, 2000 · N283WA · Boeing 727232 · Landing Gear Position and Warning
  > IR-ON GEAR RETRACTION LEFT GEAR RED LIGHT REMAINED ILLUMINATED CA-REPLACED GEAR ACCESSARY UNIT. PERFORMED MODULE CHECKOUT PER MM. SYSTEM CHECKS NORMAL.
- [SDR DL72E000242](https://openairdocs.org/sdr/DL72E000242.md): Charger · inoperative · Feb 1, 2000 · N283WA · Boeing 727247 · Emergency Lighting
  > EMERGENCY LIGHT ON AFT CARGO DOOR INOP. REPLACED BATTERY CHARGER.
- [SDR DL72E992694](https://openairdocs.org/sdr/DL72E992694.md): Bracket · cracked · Dec 9, 1999 · N283WA · Boeing 727247 · Leading Edge Devices
  > NR 8 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED ON WEB. REPAIRED PER MM 57-20-21.
- [SDR DL72E992691](https://openairdocs.org/sdr/DL72E992691.md): Angle · cracked · Dec 9, 1999 · N283WA · Boeing 727247 · Leading Edge Devices
  > DOUBLER CRACKED AT NR 2 L/E SLAT COVE SKIN ANGLE BELOW I/B UPSTOP PAD. REPAIRED PER MM 57-54-0.
- [SDR DL72E990874](https://openairdocs.org/sdr/DL72E990874.md): Oil Screen · leaking · Apr 22, 1999 · N283WA · Boeing 727247 · Turbine Engine Oil System
  > NR 3 ENG OIL ZERO, SHUT DOWN ENG. FOUND MAIN OIL SCREEN LEAKING. REPLACED MAIN OIL SCREEN AND O-RING SEAL PER MM 71-00 PG 212L AND 212M. NO LEAKS ON ENG RUN.
- [SDR DL72E990783](https://openairdocs.org/sdr/DL72E990783.md): Battery · discharged · Apr 10, 1999 · N283WA · Boeing 727247 · Emergency Lighting
  > LT AFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATT M955. OPS CHKS GOOD.
- [SDR DL72E980998](https://openairdocs.org/sdr/DL72E980998.md): Battery Pack · discharged · May 11, 1998 · N283WA · Boeing 727247 · Emergency Lighting
  > ON L/O CK, FOUND EXIT SIGNS AT CEILING BULLNOSE L1023A AND L1022A INOP W/EMER LIGHT TEST. REPLACED RACK AND BATTERY PACK PER M/M, OPN CKS OK.
- [SDR DL72E980997](https://openairdocs.org/sdr/DL72E980997.md): Battery Pack · discharged · May 11, 1998 · N283WA · Boeing 727247 · Emergency Lighting
  > ON L/O CK, FOUND O/W EXIT SIGNS OVER LT EXITS INOP W/EMERG LIGHT TEST. REPLACED RACK AND BATTERY PACK M 1090 PER M/M, OPN CKS OK.
- [SDR DL72E980585](https://openairdocs.org/sdr/DL72E980585.md): Web · cracked · Mar 16, 1998 · N283WA · Boeing 727247 · Wing, Center Box
  > THE CENTER WING FUEL TANK SPANWISE BEAM NR 1 WEB WAS FOUND CRACKED AT APPROX LBL 3, JUST BELOW THE CHEM-MILL RADIUS. THE RESULTING CUTOUT IS 2.9 (INB'D-OUTB'D) BY 0.5. REPAIRED PER ERA 331472-14.
- [SDR DL72E980545](https://openairdocs.org/sdr/DL72E980545.md): Skin · cracked · Mar 9, 1998 · N283WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > EXISTING REPAIR AT L1 DOOR LWR HINGE WAS INSTALLED PER B727 MM 53-30-00. REPAIR PER ERA 304060-14, REV B.
- [SDR DL72E981711](https://openairdocs.org/sdr/DL72E981711.md): Spar · cracked · Mar 6, 1998 · N283WA · Boeing 727247 · Trailing Edge Flaps
  > CRACK AFT SPAR RAIL DOUBLER 38 FROM I/B END OF FLAP. AFT SPAR AND SEAL RETAINER DAMAGED 33 FROM O/B END OF FLAP AFT SPAR RAIL CRACKED 55 FROM I/B END OF FLAP. ALL REPAIRED PER M/M 57-52-0 FIG 802 REF N/R CARDS 005808, 005812 AND 005810.
- [SDR DL72E981670](https://openairdocs.org/sdr/DL72E981670.md): Skin · cracked · Mar 6, 1998 · N283WA · Boeing 727247 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, A CRACK WAS DISCOVERED AT THE CORNER OF THE CUTOUT IN THE COVE SKIN FOR THE I/B AFT FLAP DRIVE ROD. THE COVE SKIN WAS REPAIRED PER MM 57-52-0 FIG 809 BY REMOVING THE DAMAGE AND INSTALLING A FILLER AND DOUBLER.
- [SDR DL72E980637](https://openairdocs.org/sdr/DL72E980637.md): Rib · cracked · Feb 25, 1998 · N283WA · Boeing 727247 · Trailing Edge Flaps
  > DURING SHOP VISIT, THE FLAP WAS FOUND WITH A CRACKED RIB AT THE LOWER AFT CORNER. THE RIB WAS REPAIRED PER 727 MM 57-52-0 FIG 808 BY STOP DRILLING THE CRACK AND INSTALLING A DOUBLER.
- [SDR DL72E981734](https://openairdocs.org/sdr/DL72E981734.md): Angle · cracked · Feb 23, 1998 · N283WA · Boeing 727247 · Trailing Edge Flaps
  > DURING SHOP VISIT THE AFT CHORD ANGLE WAS FOUND CRACKED IN 3 LOCATIONS 19, 33 AND 37 FROM I/B END OF FLAP. THE ANGLE WAS REPAIRED PER MM 57-52-0, FIG 802 BY REMOVING DAMAGED SECTION OF ANGLE AND SPLICING IN A NEW SECTION.
- [SDR DL72E980573](https://openairdocs.org/sdr/DL72E980573.md): Frame · cracked · Feb 20, 1998 · N283WA · Boeing 727247 · Fuselage Main, Frame
  > MAIN CABIN STA 930 STRINGER S-13-R FRAME CRACKED. REPAIRED PER 53-10-4 FIG 25 AND ERA 331494.
- [SDR DL72E980572](https://openairdocs.org/sdr/DL72E980572.md): Bracket · cracked · Feb 20, 1998 · N283WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > MAIN CABIN STA 930 STRINGER S-14-L BRACKET CRACKED IN RADIUS. TRIMMED OFF DAMGED SECTION OF FRAME AND BEGAN DRILLING REPAIR PER SRM 53-10-4 FIG 25. DRILLED UP REPAIR PER SRM 53-10-4 FIG 25. INSTALLED REPAIR PER SRM 53-10-4 FIG 25.
- [SDR DL72E980571](https://openairdocs.org/sdr/DL72E980571.md): False Spar · cracked · Feb 20, 1998 · N283WA · Boeing 727247 · Wing Miscellaneous Structure
  > JUST O/B OF NR 5 FLAP TRACK MOUNT, LOWER CAP OF FALSE SPAR IS CRACKED. REPAIRED PER MM 57-55-0 FIG 805.
- [SDR DL72E980565](https://openairdocs.org/sdr/DL72E980565.md): Tip · missing · Feb 20, 1998 · N283WA · Boeing 727247 · Elevator Structure
  > OB AFT TIP IS MISSING ON THE LT ELEVATOR. REMOVED DAMAGED SKIN. FABRICATED REPAIR PER M/M 55-20-0 PG 801. OK TO INSTALL. INSTALLED REPAIR PER M/M 55-20-0 PG 801.
- [SDR DL72E980299](https://openairdocs.org/sdr/DL72E980299.md): Skin · cracked · Feb 3, 1998 · N283WA · Boeing 727247 · Vertical Stabilizer, Plate/Skin
  > FOUND DURING B-1 LETTER CHECK, 1.3125 INCH CRACK VERTICAL STAB SKIN AT BASE LT SIDE JUST ABOVE FUSELAGE STA 1340. REPAIRED PER M/M 55-30-0.
- [SDR DL72E980297](https://openairdocs.org/sdr/DL72E980297.md): Web · cracked · Feb 3, 1998 · N283WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND ON B1 LETTER CK,.25 INCH CRACK IN LIGHTENING HOLE LT VERT TORQUE BOX WEB. ROUTED OUT DAMAGED AREA PER MM 53-11-0.
- [SDR DL72E980208](https://openairdocs.org/sdr/DL72E980208.md): Battery Pack · discharged · Jan 23, 1998 · N283WA · Boeing 727247 · Emergency Lighting
  > TRACK LIGHTING INOP IN FIRST CLASS. REPLACED BATTERY PACK, CKS GOOD.
- [SDR DL72E962598](https://openairdocs.org/sdr/DL72E962598.md): Bracket · cracked · Nov 26, 1996 · N283WA · Boeing 727247 · Leading Edge Slat Actuator
  > FOUND ON A1 LETTER CK, NR 1 L/E FLAP ACTUATOR I/B ATTACH BRACKET CRACKED. REPAIRED PER MM 57-20-21.
- [SDR DL72E962049](https://openairdocs.org/sdr/DL72E962049.md): Door Frame · elongated holes · Aug 23, 1996 · N283WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUR FASTENER HOLES FOUND ELONGATED ON THE STA 760.95 RT OVERWING EXIT FRAME. THESE HOLES WILL BE OVERSIZED PER B727 S/B 53-01-97, REVISION 2.
- [SDR DL72E961142](https://openairdocs.org/sdr/DL72E961142.md): Stringer · cracked · May 13, 1996 · N283WA · Boeing 727247 · Vertical Stabilizer
  > STRINGER CRACKED INSIDE TAIL CRAWLWAY 3RD BAY FROM TOP LT SIDE. REPAIRED PER MM 55-30-0 FIG 803.
- [SDR DL72E961141](https://openairdocs.org/sdr/DL72E961141.md): Frame · cracked · May 13, 1996 · N283WA · Boeing 727247 · Service Doors
  > A.375 INCH VISUAL CRACK R-2 DOOR UPPER HINGE CUTOUT AT FWD FRAME. REPAIRED PER SRM 52-40-2.
- [SDR DL72E954786](https://openairdocs.org/sdr/DL72E954786.md): Battery · discharged · Dec 19, 1995 · N283WA · Boeing 727247 · Emergency Lighting
  > DURING STANDBY POWER CHECK, FIRST CLASS EMERGENCY FLOOR LIGHTS FAILED TO ILLUMINATE. REPLACED BATTERY PACK OPERATION NORMAL.
- [SDR DL72E954676](https://openairdocs.org/sdr/DL72E954676.md): Trunnion · corroded · Dec 11, 1995 · N283WA · Boeing 727247 · Fuselage, Landing Gear Attach Fittings
  > CORROSION ON ATTACH POINTS FOR NLG TRUNNION AT MATING SURFACE FOR CAPS AND SURFACE WHERE BEARINGS SET. REPAIRED PER MM 53-40-0.
- [SDR DL72E960315](https://openairdocs.org/sdr/DL72E960315.md): Rib · cracked · Oct 9, 1995 · N283WA · Boeing 727247 · Leading Edge Devices
  > DURING SHOP INSPECTION, RIBS NR 2 AND NR 3 WERE FOUND TO BE CRACKED. REPAIRS WERE MADE AS PER M/M 57-54-0. ALSO, THE LOWER FORWARD SKIN ATTACH ANGLE WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0, FOR NR 7 L/E SLAT.
- [SDR DL72E953915](https://openairdocs.org/sdr/DL72E953915.md): Angle · cracked · Oct 4, 1995 · N283WA · Boeing 727247 · Leading Edge Devices
  > DURING F-1 LETTER CHECK, FOUND 1 INCH CRACK NR 3 L/E SLAT COVE SKIN ATTACH ANGLE BELOW ACTUATOR ATTACH POINT. REPAIRED PER M/M 57-54-0.
- [SDR DL72E953336](https://openairdocs.org/sdr/DL72E953336.md): Skin · dented · Jul 18, 1995 · N283WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > DUE TO GROUND DAMAGE, THE RIGHT SIDE OF THE FUSELAGE SUSTAINED DAMAGE. STRINGER 21R WAS SEVERED, THE SKIN DAMAGE WAS CUTOUT BETWEEN FS 660 TO FS 680 TO THE DIMENSIONS 22.5 FORE-AFT BY 20 UP AND DOWN. THE DAMAGED SECTION OF 21R HAS BEEN REMOVED FROM FS 650 TO
- [SDR DL72E951581](https://openairdocs.org/sdr/DL72E951581.md): Torque Box · cracked · Mar 28, 1995 · N283WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > AT THE LETTER CHECK, THE RT TORQUE BOX UPPER TRANSVERSE BEAM AND SUPPORT ANGLE AT FS 1273 AND THE UPPER TRANSVERSE CHANNEL AT FS 1263 WERE FOUND CRACKED. REPAIRED PER DL ERA 301422-14.
- [SDR DL72E951288](https://openairdocs.org/sdr/DL72E951288.md): Skin · cracked · Mar 27, 1995 · N283WA · Boeing 727247 · Elevator, Plate/Skin
  > ONE INCH CRACK IN LOWER LT ELEV SKIN AFT OF NR 4 BAL BOARD. FOUND DURING E-2 LTR CK TPAMM 3/27/95. INSTALLED DOUBLER PER SRM 55-20-3 FIG 4.
- [SDR DL72E951287](https://openairdocs.org/sdr/DL72E951287.md): Slat · cracked · Mar 27, 1995 · N283WA · Boeing 727247 · Leading Edge Devices
  > NUMBER 5 SLAT CRACKED AT NOSE RIBS WHERE ACT ROD END ATTACHES. FOUND DURING E-2 LETTER CHECK TPAMM 3/27/95. FOUND PREVIOUS DOUBLERS CRACKED. REPLACED SLAT ASSEMBLY.

Next page: https://openairdocs.org/deregistered/N283WA-2006-11-07/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 = 'N283WA' AND deregistration_id = 'N283WA-2006-11-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N283WA-2006-11-07/reports

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