# Service difficulty reports: N951WP, cancelled Oct 12, 2005

A list on [N951WP, cancelled Oct 12, 2005](https://openairdocs.org/deregistered/N951WP-2005-10-12.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 · 67 reports

- [SDR DL733040691](https://openairdocs.org/sdr/DL733040691.md): Wire · shorted · Jul 25, 2004 · N951WP · Boeing 7373B7 · Ignition System Wiring
  > ON DESCENT, CREW SAW SPARK AND HEARD POP COMING FROM THE WHISKEY COMPASS. COPILOT EXTENDING COMPASS AND RECEIVED SMALL SHOCK. NO FURTHER ARCING AND NO DEFECTS WERE NOTED FOR REMAINDER OF DESCENT. DELTA MTC FOUND WHISKEY COMPASS LIGHTING WIRE SHORTED TO LT EN
- [SDR DL733030933](https://openairdocs.org/sdr/DL733030933.md): Acm · failed · Oct 18, 2003 · N951WP · Boeing 7373B7 · Cabin Cooling System
  > ON CLIMBOUT FROM SLC UNABLE TO MAINTAIN PRESSURIZATION ON ONE PACK - LT PACK ON MCO FOR LOW FLOW - HISTORY ITEM. REPLACED LT ACM AND ACM DISCHARGE TEMP SW, RAN PACK CK GOOD. PRESSURIZED A/C CK GOOD.
- [SDR DL733030553](https://openairdocs.org/sdr/DL733030553.md): Coffeemaker · leaking · Jun 17, 2003 · N951WP · Boeing 7373B7 · Buffet/Galleys
  > ELEC ODOR COMING FROM FWD GALLEY COFFEEMAKER UNIT WAS TURNED OFF AND CB'S OPENED ODOR WENT AWAY. REMOVED COFFEEMAKER FOR INSPECTION FOUND WATER LEAK AT WATER SUPPLY TO HEATING TANK SECURED B-NUT DRIED ENTIRE DISPENSER CAVITY REINSTALLED BREWED TWICE THROU
- [SDR DL733030519](https://openairdocs.org/sdr/DL733030519.md): Skin · cracked · Jun 5, 2003 · N951WP · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND WITH A 3 INCH CRACK AT FS 727D JUST ABOVE STRINGER 23R RUNNING ALONG THE BONDED DOUBLER EDGE. THE CRACK WAS REMOVED WITH A 4 X 1 INCH CUTOUT AND REPAIRED WITH 2 EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 385208-14, REV B.
- [SDR DL733030275](https://openairdocs.org/sdr/DL733030275.md): Light · damaged · Mar 24, 2003 · N951WP · Boeing 7373B7 · Emergency Lighting
  > FOUND CABIN EMERGENCY EXIT LIGHT INOP AT SEAT 24DEF. REPLACED WIRE CONNECTORS AT LIGHT ASSY. OPS CHECKS NORMAL.
- [SDR DL733030266](https://openairdocs.org/sdr/DL733030266.md): Proximity Sensor · malfunctioned · Mar 22, 2003 · N951WP · Boeing 7373B7 · Engine Thrust Reverser
  > NR 2 T/R LIGHT ILLUMINATED CLIMBING THROUGH 12,000 FT. RETURN TO SLC QRH PROCEDURES COMPLIED WITH. REVERSER LIGHT ON OVERHEAD PANEL. ATB. CLEANED SIX PROXIMITY SENSORS FOR THE LEFT AND RIGHT T/R HALVES. CLEANED CANNON PLUGS FOR RIGHT AND LEFT SYNC LOCKS.
- [SDR DL733030030](https://openairdocs.org/sdr/DL733030030.md): Rod Bolt · missing · Jan 6, 2003 · N951WP · Boeing 7373B7 · Fasteners
  > L1 DOOR WOULD NOT OPEN FROM EITHER INSIDE OR OUTSIDE. FOUND LOWER LATCH AND GATE CONTROL ROD BOLT MISSING. INSTALLED CONTROL ROD BOLT. RE- INSTALLED TRIM AND SLIDE, DROPS CKS NORMAL.
- [SDR DL733021199](https://openairdocs.org/sdr/DL733021199.md): Spar · cracked · Oct 14, 2002 · N951WP · Boeing 7373B7 · Wing Spar
  > INSPECTION OF THE MLG BEAM ATTACH FITTINGS AND REAR SPAR ON THE LT WING REVEALED 6 HOLES COMMON TO THE FITTINGS AND SPAR WITH CRACK INDICATIONS. ADDITIONAL HOLES WERE DAMAGED OR ELONGATED DURING REWORK OF AREA. THE HOLES WERE OVERSIZED TO REMOVE ALL CRACKS A
- [SDR DL733020193](https://openairdocs.org/sdr/DL733020193.md): Fan · malfunctioned · Feb 15, 2002 · N951WP · Boeing 7373B7 · Air Distribution Fan
  > WHILE SITTING AT GATE NOTICED SMOKE/SMELL IN AFT CABIN. GROUND PERSONNEL STATED SMOKE CAME FROM EQUIP COOLING FAN EXHAUST. MTC INSPECTED ALL AREAS WHERE EQUIP COOL AIR DRAWN WITH NO ABNORMALITIES. RAN ENGINES AND ALL ASSOCIATED SYSTEMS, NO TROUBLE FOUND.
- [SDR DL733010396](https://openairdocs.org/sdr/DL733010396.md): Sensor · failed · Mar 11, 2001 · N951WP · Boeing 7373B7 · Cabin Pressure Control System
  > IR - AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. CABIN CLIMBED AT 1500-2000 FPM. OUTFLOW VLV SHOWED FULL CLOSED AND STBY MODE NO CHANGE. CABIN PRESSURE STABILIZED AT SAME FLT LEVEL. CA - FOUND RIGHT PACK 35 DEGREE TEMP INOP. REPLACED SAME.
- [SDR DL733002318](https://openairdocs.org/sdr/DL733002318.md): Skin · cracked · Nov 28, 2000 · N951WP · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / AFT GALLEY DOOR CUTOUT / LWR HINGE CUTOUT:CRACK REPAIR. THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR OPENING SURROUND SKIN WAS FOUND WITH A TYPICAL CRACK. THE CRACK WAS IN THE SKIN AND BONDED DOUBLER ONLY WITH NO CRACKING IN THE BEAR
- [SDR DL733002037](https://openairdocs.org/sdr/DL733002037.md): Fitting · cracked · Oct 16, 2000 · N951WP · Boeing 7373B7 · Wing, Landing Gear Attach Fittings
  > INSPECTION OF THE RT WING MLG BEAM OUTBOARD ATTACH FITTING REVEALED A CRACK EMANATING FROM A FASTENER HOLE COMMON TO THE REAR SPAR UPPER CHORD. INSPECTION OF THE BOLT HOLE REVEALED TOOLING DAMAGE COMMON TO THE REAR SPAR CAP AND WEB. THE HOLE WAS OVERSIZED TO
- [SDR DL733002036](https://openairdocs.org/sdr/DL733002036.md): Fitting · cracked · Oct 16, 2000 · N951WP · Boeing 7373B7 · Wing, Attach Fittings
  > THE MLG BEAM OUTBOARD AFT ATTACH FITTING WAS FOUND WITH A TYPICAL CRACK EMANATING FROM AN ATTACHMENT HOLE COMMON TO THE REAR SPAR UPPER CHORD. BOLT HOLE HFEC INSPECTION REVEALED A CRACK IN THE SPAR WEB AT THE FASTENER LOCATION. THE HOLE WAS OVERSIZED TO REMO
- [SDR DL733001255](https://openairdocs.org/sdr/DL733001255.md): Slide · dislodged · Jul 3, 2000 · N951WP · Boeing 7373B7 · Escape Slide
  > 1R DOOR ESCAPE SLIDE ON FLOOR. SLIDE PARTILLY DEPLOYED UPON REMOVAL. RPLD DOOR SLIDE.
- [SDR DL733000854](https://openairdocs.org/sdr/DL733000854.md): Engine · overtemp · Apr 28, 2000 · N951WP · Boeing 7373B7 · Engine (Turbine/Turboprop)
  > JUST AFTER ROTATION, NR 1 EGT 970 DEG WITH WARNING HORN FOR APPROX 10 SECONDS. REPLACED NR 1 ENG PER ROUTINE CARD DECK.
- [SDR DL733982622](https://openairdocs.org/sdr/DL733982622.md): Anti Ice Valve · failed · Dec 24, 1998 · N951WP · Boeing 7373B7 · Engine Anti-Icing System
  > RIGHT ENGINE ANTI-ICE FAILED CLOSED POSITION. AIR TURN BACK. REPLACED ANTI-ICE VALVE.
- [SDR DL733981597](https://openairdocs.org/sdr/DL733981597.md): Skin · cracked · Aug 3, 1998 · N951WP · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > R1 DOOR CUTOUT SKIN CRACKED AT AFT LWR CORNER. INSTALLED REPAIR PER SRM 53-10-01 FIG 202.
- [SDR DL733981588](https://openairdocs.org/sdr/DL733981588.md): Skin · gouged · Aug 1, 1998 · N951WP · Boeing 7373B7 · Fuselage Main, Plate/Skin
  > REPAIRED GOUGE ON FUSELAGE SKIN AT STA 400 BELOW STRINGER 19 LEFT PER SRM 53-00-01 FIG 210.
- [SDR W8PA980021](https://openairdocs.org/sdr/W8PA980021.md): Lamp · failed · Jan 21, 1998 · N951WP · Boeing 7373B7 · Emergency Lighting
  > DEN - AFT CABIN OVERHEAD EMERGENCY EXIT LIGHT IS INOP. REPLACED LAMP, OPS CHECK GOOD.
- [SDR W8PA980026](https://openairdocs.org/sdr/W8PA980026.md): Connector · disconnected · Jan 19, 1998 · N951WP · Boeing 7373B7 · Emergency Lighting
  > DEN - EMERGENCY TRACK LIGHT INOP AT ROW 15. RECONNECTED EMERGENCY LIGHT. OPS CHECK GOOD.
- [SDR W8PA980004](https://openairdocs.org/sdr/W8PA980004.md): Reflector · inoperative · Jan 7, 1998 · N951WP · Boeing 7373B7 · Emergency Lighting
  > DEN- R2 DOOR EXTERIOR EMERGENCY LIGHT IS INOP. REPLACED R2 DOOR EMERGENCY LIGHT REFLECTOR ASSY, OPS CHECK GOOD.
- [SDR W8PA980005](https://openairdocs.org/sdr/W8PA980005.md): Bulb · failed · Jan 6, 1998 · N951WP · Boeing 7373B7 · Emergency Lighting
  > DEN- OVERHEAD EMERGENCY LIGHT AT ROW 23 IS INOP. REPLACED BULB, OPS CHECK GOOD.
- [SDR W8PA971549](https://openairdocs.org/sdr/W8PA971549.md): Bulb · failed · Dec 21, 1997 · N951WP · Boeing 7373B7 · Emergency Lighting
  > DEN- THRESHOLD LIGHT AT L1 DOOR IS INOP. REPLACED BULB, OPS CHECK GOOD.
- [SDR W8PA971502](https://openairdocs.org/sdr/W8PA971502.md): Bulb · failed · Oct 24, 1997 · N951WP · Boeing 7373B7 · Emergency Lighting
  > DEN- EMERGENCY LIGHT AT ROW 18 IS INOP. RELAMPED EMERGENCY LIGHT AT ROW 18, OPS CHECK NORMAL.
- [SDR W8PA971430](https://openairdocs.org/sdr/W8PA971430.md): Wire · failed · Sep 12, 1997 · N951WP · Boeing 7373B7 · Light System Wiring
  > AFTER TAXI FROM HANGAR TO THE GATE, THE APU TEMP GAUGE BACKROUND LIGHT WAS FLICKERING AND THERE WAS THE SMELL OF SMOKE IN THE COCKPIT. FOUND SEVERAL WIRES CHAFED AND BURNED BEHIND P5 PANEL. REMOVED DAMAGED WIRES AND SPLICED REPLACEMENT WIRES. RE-TERMINATED
- [SDR W8PA971347](https://openairdocs.org/sdr/W8PA971347.md): Bulb · failed · Jul 23, 1997 · N951WP · Boeing 7373B7 · Emergency Lighting
  > BULLNOSE EMERGENCY EXIT LIGHT AT ROW 23 IS INOPERABLE. RELAMPED AS REQUIRED. OPS CHECK GOOD. (X)
- [SDR W8PA971166](https://openairdocs.org/sdr/W8PA971166.md): Light · loose · Jun 20, 1997 · N951WP · Boeing 7373B7 · Emergency Lighting
  > AISLE TRACK LIGHT CAME LOOSE FROM FLOOR ON RIGHT SIDE OF AIRCRAFT. RESECURED TRACK LIGHTING. (X)
- [SDR W8PA971163](https://openairdocs.org/sdr/W8PA971163.md): Cylinder · corroded · Jun 11, 1997 · N951WP · Boeing 7373B7 · Main Landing Gear Strut/Axle/Truck
  > RIGHT MLG OUTER CYLINDER TRUNNION LUG CORRODED AND CHROME PLATING CHIPPING AWAY ON THE FWD TRUNNION LUGS. REPLACED THE RT MLG OUTER CYLINDER. (M)
- [SDR W8PA971165](https://openairdocs.org/sdr/W8PA971165.md): Skin · delaminated · Jun 10, 1997 · N951WP · Boeing 7373B7 · Trailing Edge Flaps
  > LEFT INBOARD FORE FLAP HAS A SMALL DISBOND ON LOWER SKIN IN CENTER OF FLAP. REMOVED DAMAGED AREA, FABRICATED REPAIR AND INSTALLED PER SRM 51-70-10. (M)
- [SDR W8PA971156](https://openairdocs.org/sdr/W8PA971156.md): Support · corroded · Jun 4, 1997 · N951WP · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CORROSION ON STATION 986-1006, WL 208, LBL 38, AND STATION 1006-1016, LBL 38, WL 208 IN ANGLES. ORIGINAL THICKNESS 1. REMOVED CORRODED PARTS, INSTALLED NEW PARTS. (M)
- [SDR W8PA971161](https://openairdocs.org/sdr/W8PA971161.md): Floorbeam · cracked · May 29, 1997 · N951WP · Boeing 7373B7 · Fuselage Main, Floor Beam
  > FOUND CRACK THROUGH NUT PLATE HOLES ON FLOORBEAM BS 947, LBL 60, WL 208. REPAIRED FLOORBEAM PER SRM 53-60-51, 51-20-01, AND MM 51-21-21. (M)
- [SDR W8PA970679](https://openairdocs.org/sdr/W8PA970679.md): Support · corroded · May 26, 1997 · N951WP · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BS 312 - BS 328, RBL 11, WL 208. ORIGINAL THICKNESS.080 INCH. FOUND TO BE OUT OF LIMITS PER SRM 53-10-51. REMOVED AND REPLACED STIFFENER PER SRM 51-40-02. (X)
- [SDR W8PA970678](https://openairdocs.org/sdr/W8PA970678.md): Floor Support · corroded · May 26, 1997 · N951WP · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR SUPPORT BS 328 - BS 344, RBL 11, WL 208. ORIGINAL THICKNESS.080 INCH. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-20-02. (X)
- [SDR W8PA970733](https://openairdocs.org/sdr/W8PA970733.md): 'A' Frame · cracked · May 24, 1997 · N951WP · Boeing 7373B7 · Trailing Edge Flaps
  > NR 7 FLAP TRACK CANOE FAIRING A-FRAME IS CRACKED. REMOVED AND REPLACED CRACKED 'A' FRAME PER SRM 51-10-02. (M)
- [SDR W8PA971164](https://openairdocs.org/sdr/W8PA971164.md): Skin · delaminated · May 22, 1997 · N951WP · Boeing 7373B7 · Trailing Edge Flaps
  > DISBOND. REMOVED DAMAGED SKIN AND REPAIRED PER SRM 51-70-00, STEP 4. (M)
- [SDR W8PA971155](https://openairdocs.org/sdr/W8PA971155.md): Grommets · worn · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > WORN GROMMETS ON FLOORBEAM. REPLACED GROMMETS PER MM 20-10-41. (M)
- [SDR W8PA971153](https://openairdocs.org/sdr/W8PA971153.md): Support · double hole · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > DOUBLE HOLE ON FLOOR SUPPORT BS 340. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 51-40-02. (M)
- [SDR W8PA971152](https://openairdocs.org/sdr/W8PA971152.md): Support · misdrilled · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > DOUBLE HOLE ON FLOOR SUPPORT. REPAIRED PER EWO 97-0537. (M)
- [SDR W8PA971142](https://openairdocs.org/sdr/W8PA971142.md): Mopsill · corroded · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CORROSION ON AFT SERVICE DOOR MOPSILL BS 954-993, WL 208, RBL 53. ORIGINAL.071, REMOVED CORROSION FOUND TO BE OUT OF LIMITS PR 53-60-15. REMOVED AND REPLACED MOPSILL PER SRM 51-40-02. (M)
- [SDR W8PA970720](https://openairdocs.org/sdr/W8PA970720.md): Seat Track · damaged · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage, Seat/Cargo Attach Fittings
  > MECHANICAL DAMAGE ON SEAT TRACK. REPAIRED PER SRM 53-00-52. (M)
- [SDR W8PA970709](https://openairdocs.org/sdr/W8PA970709.md): Seat Track · damaged · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage, Seat/Cargo Attach Fittings
  > MECHANICAL DAMAGE ON SEAT TRACK. BLENDED DAMAGE, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-52, 51-40-02, 51-20-01. (M)
- [SDR W8PA970700](https://openairdocs.org/sdr/W8PA970700.md): Seat Track · damaged · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage, Seat/Cargo Attach Fittings
  > MECHANICAL DAMAGE ON SEAT TRACK, MARKED BETWEEN BS 540 AND BS 727 + 7 INCHES, RBL 45, WL 208. REMOVED AND REPLACED SEAT TRACK FROM BS 540 TO BS 727 + 7 INCHES, RBL 45, WL 208 PER SRM 53-00-52. (X)
- [SDR W8PA970688](https://openairdocs.org/sdr/W8PA970688.md): Seat Track · damaged · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage, Seat/Cargo Attach Fittings
  > MECHANICAL DAMAGE ON SEAT TRACK AT BS 328 - BS 480, RBL 24, WL 208. REPAIRED PER SRM 53-00-52. (X)
- [SDR W8PA970676](https://openairdocs.org/sdr/W8PA970676.md): Seat Track · damaged · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage, Seat/Cargo Attach Fittings
  > MECHANICAL DAMAGE ON SEAT TRACK. ORIGINAL THICKNESS.160 INCH. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-52. (X)
- [SDR W8PA970628](https://openairdocs.org/sdr/W8PA970628.md): Frame · gouged · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage Main, Frame
  > GOUGES IN FRAME AT FASTENER HOLE BS 400, RBL 57, WL 175. REPAIRED PER SRM 51-70-11. (X)
- [SDR W8PA970613](https://openairdocs.org/sdr/W8PA970613.md): Frame · cracked · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage Main, Frame
  > CRACK IN FRAME INNER CHORD BS 616, RBL 665, WL 201. CRACK WAS REPAIRED PER SB 737-53-1182. (X)
- [SDR W8PA970604](https://openairdocs.org/sdr/W8PA970604.md): Floor Beam · corroded · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM BS 328, LBL 50 - RBL 47, WL 208. ORIGINAL THICKNESS.080 INCH. FOUND BS 328, LBL 49 - LBL 51, WL 208 TO BE OUT OF LIMITS. REMOVED AND REPLACED UPPER CHORD PER SRM 51-40-02. (X)
- [SDR W8PA970602](https://openairdocs.org/sdr/W8PA970602.md): Web · cracked · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CRACKED WEB AT BS 1016, LBL 38, WL 208. REMOVED DAMAGED WEB, FABRICATED NEW PART, AND INSTALLED PER SRM'S 51-40-02-BS, 51-20-01, AND 51-30-01, AND MM 51-21-99. (X)
- [SDR W8PA970600](https://openairdocs.org/sdr/W8PA970600.md): Web · cracked · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage Miscellaneous Structure
  > CRACKED WEB ANGLE BS 927 - BS 947, BL ZERO, WL 208. FABRICATED, ALODINED AND PRIMED, INSTALLED REPAIR PARTS. (X)
- [SDR W8PA970598](https://openairdocs.org/sdr/W8PA970598.md): Floor Beam · corroded · May 22, 1997 · N951WP · Boeing 7373B7 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM STA 967, RBL 18, LBL 43, WL 208. ORIGINAL THICKNESS.125 INCH. REMOVED DAMAGED PARTS, FABRICATED NEW PARTS, INSTALLED PER SRM 53-00-51. (X)

Next page: https://openairdocs.org/deregistered/N951WP-2005-10-12/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 = 'N951WP' AND deregistration_id = 'N951WP-2005-10-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N951WP-2005-10-12/reports

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