# Service difficulty reports: N296WA, cancelled Nov 8, 2006

A list on [N296WA, cancelled Nov 8, 2006](https://openairdocs.org/deregistered/N296WA-2006-11-08.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 · 64 reports

- [SDR DL72W021270](https://openairdocs.org/sdr/DL72W021270.md): Relay · failed · Oct 31, 2002 · N296WA · Boeing 727247 · Emergency Lighting
  > EMERGENCY LIGHT REMAINS ON IN THE ARM POSITION. REPLACED R600, CKS OK.
- [SDR DL72W021240](https://openairdocs.org/sdr/DL72W021240.md): Bushing · worn · Oct 25, 2002 · N296WA · Boeing 727247 · Landing Gear Retraction/Extension System
  > ATB TO TPA - LANDING GEAR WOULD NOT RETRACT AFTER TAKE-OFF FOUND AIR TO GROUND SENSOR ACTUATING ARM PIVOT BUSHING - EXCESSIVE PLAY - REPLACED SAME - OPS CHECKED GOOD PER M/M
- [SDR DL72W021219](https://openairdocs.org/sdr/DL72W021219.md): Relay · intermittent · Oct 22, 2002 · N296WA · Boeing 727247 · Emergency Lighting
  > EMERGENCY LIGHTS FLICKER IN A NORMAL FLIGHT OPERATION. EFFECTED LIGHTS ARE ROW 30 AND FORWARD IN CABIN. REPLACED RELAY, OP CKS GOOD.
- [SDR DL72W021212](https://openairdocs.org/sdr/DL72W021212.md): Switch · malfunctioned · Oct 19, 2002 · N296WA · Boeing 727247 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS CAME ON AT CRUISE 1:10 MINS INTO FLIGHT. REPLACED AFT SWITCH AT FLT ATTD PANEL AND R600 EMERG EXIT RELAY. EMERGENCY EXIT LIGHTS OPS CKS NORM.
- [SDR DL72W021073](https://openairdocs.org/sdr/DL72W021073.md): Battery · discharged · Sep 13, 2002 · N296WA · Boeing 727247 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS IN OVERHEAD PANEL AT OVERWING EXIT LOCATION AND AT AFT SERVICE DOOR LOCATION INOP. REPLACED BATTERY M1094 AND BOTH BATTERY AND PACK A7 M1095, ALL CKS OK.
- [SDR DL72W020491](https://openairdocs.org/sdr/DL72W020491.md): Battery · discharged · Apr 29, 2002 · N296WA · Boeing 727247 · Emergency Lighting
  > RT OVERWING EXIT SIGN EMERGENCY LIGHTS INOP. REPLACED BATTERY, CKS OK.
- [SDR DL72W020134](https://openairdocs.org/sdr/DL72W020134.md): Transmitter · faulty · Feb 3, 2002 · N296WA · Boeing 727247 · Engine Oil Pressure
  > NR 3 OIL PRESSURE INDICATION DROPPED TO 32 PSI WHEN TAKEOFF POWER APPLIED. TAKEOFF ABORTED AT 70 KTS, GROSS WEIGHT 162.0. BRAKE COOLING IN NORMAL RANGE. REPLACED NR 3 ENGINE OIL PRESSURE TRANSMITTER, LEAK CHECKS OK. PRESSURE CHECKS NORMAL ON ENGINE RUN.
- [SDR DL72W011815](https://openairdocs.org/sdr/DL72W011815.md): Battery Pack · discharged · Nov 13, 2001 · N296WA · Boeing 727247 · Emergency Lighting
  > RIGHT AFT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK.
- [SDR DL72W011810](https://openairdocs.org/sdr/DL72W011810.md): Battery Pack · discharged · Nov 13, 2001 · N296WA · Boeing 727247 · Emergency Lighting
  > FOUND RIGHT AFT OVERWING EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK.
- [SDR DL72W011495](https://openairdocs.org/sdr/DL72W011495.md): Frame · cracked · Sep 6, 2001 · N296WA · Boeing 727247 · Fuselage Main, Frame
  > FUSELAGE / FRAME / FS 1303 / RH: CRACKED FLANGE REPAIR THE FS 1303 RH FRAME WAS FOUND WITH A CRACK IN THE INNER FLANGE OF THE FRAME AT A HYDRAULIC LINE CLAMP ATTACH LOCATION JUST ABOVE
- [SDR DL72W011490](https://openairdocs.org/sdr/DL72W011490.md): Angle · cracked · Sep 5, 2001 · N296WA · Boeing 727247 · Fuselage Structure (General)
  > 1 IN. CRACK GUSSET ANGLE AFT SIDE STA 1263 R/H TORQUE BOX REPAIRED PER M/M 53-11-000-8
- [SDR DL72W020879](https://openairdocs.org/sdr/DL72W020879.md): Sign · inoperative · Jul 27, 2001 · N296WA · Boeing 727247 · Emergency Lighting
  > LEFT SIDE EMERGENCY WINDOW EXITS SIGNS NEED TO BE RELAMPED. RELAMPED AS REQUIRED.
- [SDR DL72W010879](https://openairdocs.org/sdr/DL72W010879.md): Power Supply · discharged · May 31, 2001 · N296WA · Boeing 727247 · Emergency Lighting
  > AFT 6 ROWS OF SEATS EMERGENCY LIGHTS INOP AND R2 DOOR EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY.
- [SDR DL72W010302](https://openairdocs.org/sdr/DL72W010302.md): Battery · discharged · Feb 20, 2001 · N296WA · Boeing 727247 · Emergency Lighting
  > L1 DOOR OVERHEAD EMERGENCY LIGHT BATTERY DEAD. REPLACED LIGHT ASSY.
- [SDR DL72W010257](https://openairdocs.org/sdr/DL72W010257.md): Skin · cracked · Feb 12, 2001 · N296WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 & 681 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONFIRMED 11 CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN ALONG THE LENGTH OF THE LAP JOINT. THE ENTIRE SKIN LAP WAS CUTOUT AND REPAIRED
- [SDR DL72W010254](https://openairdocs.org/sdr/DL72W010254.md): Skin · cracked · Feb 12, 2001 · N296WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 26L SKIN LAP JOINT BETWEEN FS 480 & 680 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONFIRMED MULTIPLE CRACKS IN THE LOWER SKIN AT THE LOWER FASTENER ROW. THE ENTIRE LAP JOINT WAS CUTOUT TO REMOVE ALL CRACKS. THE JOINT WAS R
- [SDR DL72W010232](https://openairdocs.org/sdr/DL72W010232.md): Skin · cracked · Feb 8, 2001 · N296WA · Boeing 727247 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP JOINT INDICATED CRACKS BETWEEN FS 680 & 740. INTERNAL MFEC INSPECTION CONFIRMED 5 CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. THE ENTIRE SKIN LAP SPLICE WAS CUT AWAY TO REMOVE ALL DAMAGE. THE LAP WAS RESTO
- [SDR DL72W010122](https://openairdocs.org/sdr/DL72W010122.md): Skin · cracked · Jan 23, 2001 · N296WA · Boeing 727247 · Leading Edge Devices
  > A 1 INCH CRACK AT NR 2 SLAT LWR COVE SKIN ANGLE O/B END. REPAIRED PER MM 57-54-0.
- [SDR DL72W002105](https://openairdocs.org/sdr/DL72W002105.md): Battery · inoperative · Oct 24, 2000 · N296WA · Boeing 727247 · Emergency Lighting
  > EMERGENCY LIGHT AFT OF RIGHT I/B FLAP INOP. REMOVED AND REPLACED POWER SUPPLY AND BATTERY. OPS CHECK GOOD.
- [SDR DL72W002104](https://openairdocs.org/sdr/DL72W002104.md): Battery · inoperative · Oct 24, 2000 · N296WA · Boeing 727247 · Emergency Lighting
  > CEILING EMERGENCY LIGHT AT ROW 13 INOP. REMOVED AND REPLACED LIGHT ASSEMBLY AND BATTERY, OPS CHECKS GOOD.
- [SDR DL72W001862](https://openairdocs.org/sdr/DL72W001862.md): Rib · cracked · Sep 22, 2000 · N296WA · Boeing 727247 · Wing, Rib/Bulkhead
  > THE BL 70.5 RIB CHORDS ON THE LT & RT WINGS WERE FOUND WITH TYPICAL FASTENER HOLE CRACKS IN THE VERTICAL FLANGE OF THE CHORDS AT FS 760.95. THE CRACKS ARE THE FWD FASTENER HOLE OF EACH CHORD AND ARE TYPICAL OF BAC S/B 727-57-0112. THE CRACKS WERE REMOVED BY
- [SDR DL72W001861](https://openairdocs.org/sdr/DL72W001861.md): Frame · corroded · Sep 22, 2000 · N296WA · Boeing 727247 · Fuselage Main, Frame
  > THE OUTBOARD CHORD OF THE C1 DOOR CUTOUT LOWER SILL BEAM (STR 26R) WAS FOUND WITH DEEP CORROSION ON THE OUTBOARD FLANGE JUST AFT THE THE FS 620 FRAME. THE DAMAGED SECTION OF FLANGE WAS TRIMMED OUT. THE CHORD WAS REPAIRED WITH TWO EXTERNAL ALUMINUM REPA
- [SDR DL72W001759](https://openairdocs.org/sdr/DL72W001759.md): Stringer · cracked · Sep 8, 2000 · N296WA · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > ONE HALF INCH CRACK ON HORIZONTAL FLANGE OF STRINGER 18A, LEFT HAND SIDE AT STATION 950 (APPROX). INSTALLED LEVEL II TIME-LIMITED REPAIR PER MAINTENANCE MANUAL 53-12-0.
- [SDR DL72W001158](https://openairdocs.org/sdr/DL72W001158.md): Trunnion · corroded · Jun 14, 2000 · N296WA · Boeing 727247 · Main Landing Gear Attach Section
  > THE I/B LUG OF THE LEFT MAIN LANDING GEAR TRUNNION SUPPORT BEAM WAS FOUND CORRODED. THE LUG BORE WAS OVERSIZED TO REMOVE THE CORROSION AND AN OVERSIZED REPAIR BUSHING WAS INSTALLED. THE REPAIR WAS ACCOMPLISHED PER ER/A 377531-14.
- [SDR DL72W001044](https://openairdocs.org/sdr/DL72W001044.md): Radar · malfunctioned · May 28, 2000 · N296WA · Boeing 727247 · Weather Radar System
  > RADAR DID NOT WORK AIRBORNE. GOOD TEST ON DECK. TURNED ON IN AIR ONLY GOT SPOKES. TURNED OFF (RECYCLED) SAME RESULTS. REPLACED WEATHER RADAR INDICATOR. GROUND TEST OK, CHECKED UNDER NORMAL MAP OPERATION CHECKS OK.
- [SDR DL72W992728](https://openairdocs.org/sdr/DL72W992728.md): Radar · failed · Dec 13, 1999 · N296WA · Boeing 727247 · Independent Position Determining System
  > AIRBORNE THE RADAR WOULD NOT PAINT ANY GROUND OR WX, BUT WOULD OCCASIONALLY SPIKE. REPLACED RT UNIT.
- [SDR DL72W992649](https://openairdocs.org/sdr/DL72W992649.md): Light · inoperative · Dec 4, 1999 · N296WA · Boeing 727247 · Emergency Lighting
  > FWD AND AFT RT OVERWING EMERGENCY LIGHTS INOP. REPLACED RACK, OP CKS GOOD.
- [SDR DL72W990884](https://openairdocs.org/sdr/DL72W990884.md): Angle · cracked · Apr 23, 1999 · N296WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > TORQUE BOX HORIZONTAL Z ANGLE CRACKED AT STA 1273. TORQUE BOX HORIZONTAL ANGLE FWD SIDE OF Z ANGLE CRACKED AT STA 1273. REPLACED PARTS PER SRM 53-10-10.
- [SDR DL72W990617](https://openairdocs.org/sdr/DL72W990617.md): Coupling · failed · Mar 23, 1999 · N296WA · Boeing 727247 · Trailing Edge Flap Control System
  > DURING APPROACH TO ATL, UPON SEL 5 DEG FLAPS THE OUTBOARD NEEDLES SPLIT AND REMAINED AT 2 DEG. FOUND LT OUTBOARD T/E FLAP DRIVE (TORQUE) TUBE COUPLING, FAILED JUST INBOARD OF LT MLG SPAR.
- [SDR DL72W990390](https://openairdocs.org/sdr/DL72W990390.md): Actuator · failed · Feb 25, 1999 · N296WA · Boeing 727247 · Leading Edge Slat Actuator
  > NR 4 SLAT DID NOT RETRACT. C/W POM. VISUALLY CONFIRMED. REPLACED NR 4 SLAT ACTUATOR.
- [SDR DL72W982445](https://openairdocs.org/sdr/DL72W982445.md): Actuator · damaged · Nov 26, 1998 · N296WA · Boeing 727247 · Leading Edge Slat Actuator
  > NR 3 L/E SLAT ACTUATOR CASE FAILURE, RESULTING IN LOSS OF A-SYS HYD POWER. REPLACED ACTUATOR.
- [SDR DL72W982411](https://openairdocs.org/sdr/DL72W982411.md): Battery Pack · discharged · Nov 21, 1998 · N296WA · Boeing 727247 · Emergency Lighting
  > ON L/O, FOUND INTERNAL OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK, EMERGENCY LIGHTS NOW CHECK NORMAL PER M/M.
- [SDR DL72W982079](https://openairdocs.org/sdr/DL72W982079.md): Angle · corroded · Oct 7, 1998 · N296WA · Boeing 727247 · Nacelle/Pylon Structure
  > WHILE PERFORMING HUSH-KIT MOD, FOUND RT CHORD ANGLE ON NR 2 ENG SLOPING WEB CORRODED BEYOND MFG SPECS. REPLACED RT CHORD WITH NEW SCV CHORD.
- [SDR DL72W982078](https://openairdocs.org/sdr/DL72W982078.md): Angle · corroded · Oct 5, 1998 · N296WA · Boeing 727247 · Nacelle/Pylon Structure
  > FOUND LT CHORD ANGLE ON NR 2 ENG SLOPING WEB WITH CORROSION BEYOND MFG SPECS. REPLACED CHORD ANGLE WITH NEW CHORD ANGLE.
- [SDR DL72W981920](https://openairdocs.org/sdr/DL72W981920.md): Web · cracked · Sep 15, 1998 · N296WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > REF SHIP 588 TPA LTR CHECK B-2,.25 INCH CRACK AT LIGHTENING HOLE 8AFT OF LT AIRSTAIR UPSTOP PAD. ROUT OUT AND TREAT PER MM 53-11-0.
- [SDR DL72W980454](https://openairdocs.org/sdr/DL72W980454.md): Skin · cracked · Feb 23, 1998 · N296WA · Boeing 727247 · Wing, Plate/Skin
  > THE RMLG BEAM WAS DISCOVERED TO HAVE SEVERAL DAMAGE LOCATIONS. THE NR 2 SKIN PANEL ATTACH HOLE ON THE LWR FLANGE OF THE BEAM WAS FOUND WITH A CRACK IN THE BORE. THE OUTBD MLG SUPPORT LUG HOLE WAS FOUND CORRODED AND THE UNDERSIDE OF THE LWR FLANGE OF THE BEAM
- [SDR DL72W980453](https://openairdocs.org/sdr/DL72W980453.md): Sill · corroded · Feb 23, 1998 · N296WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > THE C2 DOOR CUTOUT LOWER SILL WAS FOUND WITH CORROSION ON THE OUBTBD FLANGE OF THE OUTBD CHORD. REPAIRED PER ERA 331330-14.
- [SDR DL72W980452](https://openairdocs.org/sdr/DL72W980452.md): Spar · misdrilled · Feb 23, 1998 · N296WA · Boeing 727247 · Elevator, Spar/Rib
  > DURING ACCOMPLISHMENT OF THE REAR SPAR MOD ON THE LT ELEVATOR IT WAS NOTED THAT SEVERAL HOLES WERE OVERSIZED. REPAIRED PER ERA 331369-14AD.
- [SDR DL72W980354](https://openairdocs.org/sdr/DL72W980354.md): Blkhd Stiffener · cracked · Feb 10, 1998 · N296WA · Boeing 727247 · Fuselage Main, Bulkhead
  > CRACKS WERE FOUND IN THE L/RBL 36083 VERT STIFFENER ON THE FWD SIDE OF THE BS 1183 BLKHD. CRACKS WERE LOCATED AT APPROX WL 238 AND WERE NO MORE THAN 2 IN LENGTH. REPAIR PER ERA 331332-14.
- [SDR DL72W980341](https://openairdocs.org/sdr/DL72W980341.md): Bulkhead Beam · cracked · Feb 9, 1998 · N296WA · Boeing 727247 · Fuselage Main, Bulkhead
  > MTC FOUND A.1875 INCH CRACK IN THE OUTBD AFT FLANGE OF THE RBL 8 VERT BEAM IN THE FS 1183 BLKHD, WHICH BEGINS AT WL 182. REPAIRED PER ERA 362891-14, REV A.
- [SDR DL72W980358](https://openairdocs.org/sdr/DL72W980358.md): Angle · cracked · Feb 5, 1998 · N296WA · Boeing 727247 · Trailing Edge Flaps
  > DURING SHOP, THE AFT SPAR ANGLE WAS FOUND CRACKED 34 FROM THE IB END OF THE FLAP. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 802.
- [SDR DL72W980357](https://openairdocs.org/sdr/DL72W980357.md): Angle · cracked · Feb 5, 1998 · N296WA · Boeing 727247 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT SPAR ANGLE WAS FOUND CRACKED 18 FROM IB END OF FLAP. THE ANGLE WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 802.
- [SDR DL72W980346](https://openairdocs.org/sdr/DL72W980346.md): Fitting · corroded · Feb 4, 1998 · N296WA · Boeing 727247 · Wing, Fuselage Attach Fittings
  > CORROSION RT AFT WING TERMINAL FITTING AFT BUSHING BORE. BORED FITTING BORE TO 4.500 PER SRM 53-40-01 TO REMOVE CORROSION. TURNED BUSHING TO PROPER FIT. TREATED BUSHING. OK TO TREAT FITTING BORE. TREATED BORE, OK TO INST SLEEVE. INSTALLED SLEEVE PER SRM
- [SDR DL72W980356](https://openairdocs.org/sdr/DL72W980356.md): Angle · cracked · Jan 30, 1998 · N296WA · Boeing 727247 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT SPAR ANGLE WAS FOUND CRACKED 37 FROM THE I/B END OF FLAP. THE CRACK WAS REPAIRED BY INSTALLING A DOUBLER PER 727 MM 57-52-0, FIG 802.
- [SDR DL72W980345](https://openairdocs.org/sdr/DL72W980345.md): Box · corroded · Jan 27, 1998 · N296WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > WING ICE LIGHT BOX BETWEEN STA 720B AND 720C AT STR 15L IS CORRODED. REPAIRED PER SRM 53-30-3 FIG 22.
- [SDR DL72W972523](https://openairdocs.org/sdr/DL72W972523.md): Tire · out of round · Dec 2, 1997 · N296WA · Boeing 727247 · Tire
  > EXCESSIVE VIBRATION FROM NOSE WHEEL AT ROTATION VR AT 145KTS, NO ABNORMAL INDICATIONS. FOUND RT NOSE TIRE OUT OF ROUND. REPLACED SAME.
- [SDR DL72W972165](https://openairdocs.org/sdr/DL72W972165.md): Battery Pack · discharged · Oct 25, 1997 · N296WA · Boeing 727247 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ON OVERHEAD FWD OF AFT GALLEY INOP. REPLACED BATTERY PACK.
- [SDR DL72W972101](https://openairdocs.org/sdr/DL72W972101.md): Fire Test Panel · malfunctioned · Oct 18, 1997 · N296WA · Boeing 727247 · Fire Detection
  > APU FIRE BELL CAME ON IN FLT WITH NO OTHER INDICATIONS AND WOULD NOT RESET OR CUT OUT AFTER SEVERAL ATTEMPTS. FINALLY WENT OUT AFTER MOVING BELL RESET PUSH-BUTTON SIDE TO SIDE. RESEATED CONNECTORS ON FIRE DETECT TEST PANEL.
- [SDR DL72W971945](https://openairdocs.org/sdr/DL72W971945.md): Stringer · cracked · Oct 1, 1997 · N296WA · Boeing 727247 · Vertical Stabilizer
  > FOUND DURING A2 LETTER CHECK, VERT STAB STR 96 CRACKED AT FIN STA 180.6. REPAIR PER M/M 55-30-0.
- [SDR DL72W971944](https://openairdocs.org/sdr/DL72W971944.md): Angle · cracked · Oct 1, 1997 · N296WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND AT A2 LETTER CHECK, GUSSET ANGLE CRACKED RT SIDE STA 1263 BELOW STAIR ACTUATOR PAD. REPLACED ANGLE PER SRM 53-10-10.

Next page: https://openairdocs.org/deregistered/N296WA-2006-11-08/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 = 'N296WA' AND deregistration_id = 'N296WA-2006-11-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N296WA-2006-11-08/reports

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