# Service difficulty reports: N292WA, cancelled Jul 20, 2010

A list on [N292WA, cancelled Jul 20, 2010](https://openairdocs.org/deregistered/N292WA-2010-07-20.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 · 100 reports

- [SDR DL72W020883](https://openairdocs.org/sdr/DL72W020883.md): Engine · out of trim · Jul 28, 2002 · N292WA · Boeing 727247 · Engine (Turbine/Turboprop)
  > REJECTED TAKEOFF. AIRSPEED APPROX 130 KIAS LIGHT BRAKING. EVERYTHING ELSE NORMAL WITH ABORT. COULD NOT GET NORMAL POWER EPR OF 2.06 OUT OF NUMBER 1 ENGINE. N1 AND EGT NORMAL. FIRE DEPT INSPECTED BRAKES, CHECKED OK. REMOVED AND REPLACED EPR TRANSMITTER NR
- [SDR DL72W011876](https://openairdocs.org/sdr/DL72W011876.md): Angle · cracked · Nov 28, 2001 · N292WA · Boeing 727247 · Wing Structure
  > NBR 7 SLAT ANGLE CRACKED AT INBD STOP PAD ATTACH FOUND AT F1 LETTER CK REPAIRED PER MM 57-54-000-8
- [SDR DL72W011875](https://openairdocs.org/sdr/DL72W011875.md): Angle · cracked · Nov 28, 2001 · N292WA · Boeing 727247 · Wing Structure
  > NBR 8 SLAT ANGLE CRACKED AT ANTIICE T DUCT CUTOUT FOUND ON F1 LETTER CHECK REPAIRED PER MM 57-54-000-8
- [SDR DL72W011058](https://openairdocs.org/sdr/DL72W011058.md): Battery Pack · discharged · Jun 24, 2001 · N292WA · Boeing 727247 · Emergency Lighting
  > LEFT FWD AND AFT EMERGENCY EXIT EXTERIOR LIGHT INOP. REPLACED BATTERY PACKS.
- [SDR DL72W011057](https://openairdocs.org/sdr/DL72W011057.md): Battery Pack · discharged · Jun 24, 2001 · N292WA · Boeing 727247 · Emergency Lighting
  > LEFT FWD AND AFT EMERGENCY EXIT EXTERIOR LIGHTS INOP. REPLACED BATTERY PACKS.
- [SDR DL72W010952](https://openairdocs.org/sdr/DL72W010952.md): Engine · malfunctioned · Jun 12, 2001 · N292WA · Boeing 727247 · Engine (Turbine/Turboprop)
  > ON T/O ROLL, NR 3 ENG INSTR WERE UNSTABLE. ABORTED AT 110 KNOTS. ON INITIAL PWR APPLICATION NR 3 ENG WAS STABLE THEN PROGRESSIVELY BECAME UNSTABLE. NORMAL PWR USED. VERSA LUBE NR 3 ENG FUEL CONTROL. INSP MAIN CHIP DETECTOR, INSP INTAKE, EXH AND NO DEFECTS
- [SDR DL72W002230](https://openairdocs.org/sdr/DL72W002230.md): Ballast · shorted · Nov 14, 2000 · N292WA · Boeing 727247 · Passenger Compartment Lighting
  > BALLAST AT 15 ABC POPPED C/B AND EMITTED BURNING SMELL. REPLACED BALLAST. OP CKS NORMAL.
- [SDR DL72W001702](https://openairdocs.org/sdr/DL72W001702.md): Web · cracked · Aug 30, 2000 · N292WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > AT MIDVISIT, THE RT LOWER CORNER OF THE 1303 WEB WAS CRACKED. DRILLED UP DOUBLER PER DRD 53-10-4D FIG 802D. STOP DRILLED CRACK PER DRD 53-10-4D AND DYE CKED PER DRD 53-10-4D FIG 802D. NO CRACK FOUND BEYOND DOUBLER HOLE. OK TO INSTALL. INSTALLED DOUBLER PE
- [SDR DL72W001701](https://openairdocs.org/sdr/DL72W001701.md): Web · cracked · Aug 30, 2000 · N292WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > AT MIDVISIT, THE LT LWR CORNER OF 1303 WEB WAS FOUND CRACKED. DRILLED UP DOUBLER PER DRD 53-10-4 FIG 802. STOP DRILLED CRACK PER DRD 53-10-4 AND DYE CKED PER DRD 53-10-4D FIG 802, NO CRACK BEYOND STOP DRILL. OK TO INSTALL. INSTALLED DOUBLER PER DRD 53-10-4
- [SDR DL72W001762](https://openairdocs.org/sdr/DL72W001762.md): Rib · cracked · Aug 29, 2000 · N292WA · Boeing 727247 · Leading Edge Devices
  > AT MV2, RIB CRACKED NR 7 SLAT O/B RIB AT ACTUATOR ATTACH POINT. FABBED DBLR PER 727 MM 57-54-0 FIG 804, INSTALLED DBLR PER 727 MM 57-54-0 FIG 804, INSTALLED COVER PNL ON R/C 636.
- [SDR DL72W001761](https://openairdocs.org/sdr/DL72W001761.md): Rib · cracked · Aug 29, 2000 · N292WA · Boeing 727247 · Leading Edge Devices
  > AT MV2 FOUND RW RIB CRACKED NR 7 SLAT I/B RIB AT ACTUATOR ATTACH POINT. FABBD DBLR PER MM 727-57-54-0 FIG 804. INSTALLED DBLR PER MM 57-54-0 FIG 804.
- [SDR DL72W001754](https://openairdocs.org/sdr/DL72W001754.md): Rib · cracked · Aug 29, 2000 · N292WA · Boeing 727247 · Leading Edge Devices
  > AT MV2 FOUND RW RIB CRACKED NR 6 L/E SLAT, I/B RIB AT ACTUATOR ATTACH POINT. REMOVED PREV REPAIR AND FABBD REPLACEMENT DBLR PER MM 51-540 FIG 804. REPAIRED PER CMM 57-54-0 FIG 804, INSTALLED AND REMOVED ON R/C 634.
- [SDR DL72W001733](https://openairdocs.org/sdr/DL72W001733.md): Rib · cracked · Aug 29, 2000 · N292WA · Boeing 727247 · Leading Edge Devices
  > RIB-CRACKED NR 7 SLAT I/B RIB AT ACTUATOR ATTACH POINT W/W NRC 303. FABRICATED DOUBLER PER MM 727-57-54-0 FIG 804. OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER 727 MM 57-54-0 FIG 804. REMOVED AND INSTALLED ON RC 636.
- [SDR DL72W001732](https://openairdocs.org/sdr/DL72W001732.md): Rib · cracked · Aug 29, 2000 · N292WA · Boeing 727247 · Leading Edge Devices
  > RIB CRACKED NR 7 SLAT O/B RIB AT ACTUATOR ATTACH POINT W/W NRC 342. FABRICATED DOUBLER PER 727 MM 57-54-0 FIG 804 OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER 727 MM 57-54-0 FIG 804. OK TO INSTALL PANEL. INSTALLED COVE PANEL. REMOVED AND INSTALLED ON RC 6
- [SDR DL72W001301](https://openairdocs.org/sdr/DL72W001301.md): Light · failed · Jul 9, 2000 · N292WA · Boeing 727247 · Emergency Lighting
  > AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WILL NOT LIGHT. REPLACED LIGHT ASSY, OP CKS GOOD.
- [SDR DL72W992389](https://openairdocs.org/sdr/DL72W992389.md): O-Ring · leaking · Oct 28, 1999 · N292WA · Boeing 727247 · Engine Fuel Distribution
  > NR 3 ENGINE FLAMED OUT ON APPROACH AT 6000 FEET. AT LEVEL OFF 6000 FEET DURING FINAL APPROACH SEGMENT NR 3 INSTRUMENTS INDICATED THE FOLLOWING FUEL FLOW 0 / 35 PERCENT N2 / EPR0 / N1 ZERO / NORMAL OIL PRESS, NORMAL OIL TEMP / THROTTLE MOVEMENT, NO EFFECT / NR
- [SDR DL72W992340](https://openairdocs.org/sdr/DL72W992340.md): Light · inop · Oct 24, 1999 · N292WA · Boeing 727247 · Emergency Lighting
  > AFT STAIR EMERGENCY OVERHEAD LIGHT INOP. REPLACED LIGHT PACK ASSY, OPS CHECK NORMAL.
- [SDR DL72W991941](https://openairdocs.org/sdr/DL72W991941.md): Fitting · loose · Aug 31, 1999 · N292WA · Boeing 727247 · Engine Mount Section
  > ON TAKEOFF NR 1 ENG HAD LOW OIL PRESSURE AND LOW OIL PRESSURE LIGHT. ALSO, OIL QTY DROPPED. RTO FOUND BANJO FITTING LOOSE AND TIGHTEND SAME. MTC FERRY ATL FOR ENGINE CHANGE.
- [SDR DL72W990315](https://openairdocs.org/sdr/DL72W990315.md): Actuator · leaking · Feb 17, 1999 · N292WA · Boeing 727247 · Leading Edge Slat Actuator
  > INFLIGHT 'A' SYS HYD QTY DECREASED TO NEAR ZERO, ACCOMPLISHED PROD IAW POM. REPLACED INBOARD KRUEGER FLAP ACTUATOR.
- [SDR DL72W982254](https://openairdocs.org/sdr/DL72W982254.md): Battery Pack · discharged · Nov 1, 1998 · N292WA · Boeing 727247 · Emergency Lighting
  > ON L/O, FOUND EMERGENCY EXIT LIGHT OVER DOOR L2 INOP. REPLACED BATTERY PACK, OPS CKS NORMAL.
- [SDR DL72W981344](https://openairdocs.org/sdr/DL72W981344.md): Floorbeam · corroded · Jun 16, 1998 · N292WA · Boeing 727247 · Fuselage Main, Floor Beam
  > CORROSION AT FLOORBEAM STA 344 FROM LBL 13 TO RBL 17-MARKED. REPAIRED PER SRM 53-10-8 FIG 11.
- [SDR DL72W981205](https://openairdocs.org/sdr/DL72W981205.md): Power Supply · inoperative · Jun 7, 1998 · N292WA · Boeing 727247 · Emergency Lighting
  > FOUND ON LAYOVER INSP, AIRSTAIR DOOR EXIT LIGHT FLICKERING. REPLACED ASSOCIATED POWER SUPPLY.
- [SDR DL72W981026](https://openairdocs.org/sdr/DL72W981026.md): Rib · cracked · May 13, 1998 · N292WA · Boeing 727247 · Leading Edge Devices
  > FOUND ON C1 LETTER CK, L/E NOSE RIB CRACKED 1.25 INCH PAST, STOP DRILL, NR 5 SLAT ACTUATOR INBD ATTACH RIB. REPAIRED PER MM 57-54-0.
- [SDR DL72W981024](https://openairdocs.org/sdr/DL72W981024.md): Web · cracked · May 13, 1998 · N292WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND AT C1 LETTER CK, RT TORQUE BOX WEB CRACKED AT UPPER END STA 1214, REPAIRED PER M/M 53-11-0 PG 832 RT TORQUE BOX WEB CRACKED.25 INCH AT UPPER LIGHTENING HOLE STA 1225. REPAIRED PER M/M 53-11-0 PG 828.
- [SDR DL72W962602](https://openairdocs.org/sdr/DL72W962602.md): Battery Pack · discharged · Nov 28, 1996 · N292WA · Boeing 727247 · Emergency Lighting
  > DURING L/O CK, FOUND RIGHT SIDE OVERWING EXIT LIGHTS INOP. REPLACED BATTERY PACK, OPS CKS OK.
- [SDR DL72W962300](https://openairdocs.org/sdr/DL72W962300.md): Light · inoperative · Oct 11, 1996 · N292WA · Boeing 727247 · Emergency Lighting
  > FWD GALLEY DOOR REMOVABLE EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY AND BATTERIES, OPS CHECKS OK.
- [SDR DL72W962299](https://openairdocs.org/sdr/DL72W962299.md): Battery Pack · discharged · Oct 11, 1996 · N292WA · Boeing 727247 · Emergency Lighting
  > OVERWING EXIT SIGNS INOP ON RIGHT SIDE. REPLACED BATTERY PACK AT M1086, OPS CHECKS OK.
- [SDR DL72W961044](https://openairdocs.org/sdr/DL72W961044.md): Hyd Pump · inoperative · May 1, 1996 · N292WA · Boeing 727247 · Hydraulic Pump (Electric/Engine), Main
  > FLT 893 - AIR TURN BACK DUE TO B-SYSTEM HYDRAULIC WENT TO ZERO WITH LOW PRESSURE LIGHT ON. A-SYSTEM AT 2.5 GALLONS. REPLACED INBOARD B-SYSTEM HYDRAULIC PUMP AND FILTERS. REPLACED NR 5 SPOILER FILTER HOUSING PACKING. RESERVICED HYDRAULIC SYSTEM. OPS AND LE
- [SDR DL72W960127](https://openairdocs.org/sdr/DL72W960127.md): Battery Pack · discharged · Jan 19, 1996 · N292WA · Boeing 727247 · Emergency Lighting
  > DURING INSPECTION, AFT CABIN BULLNOSE EMERGENCY LIGHT INOP. REPLACED BATT RACK, OPS NORMAL.
- [SDR DL72W961585](https://openairdocs.org/sdr/DL72W961585.md): Transverse Beam · cracked · Jan 18, 1996 · N292WA · Boeing 727247 · Fuselage Miscellaneous Structure
  > THERE IS A 1 INCH CRACK IN THE ANGLE OF BOTH THE FWD AFT TRANSVERSE BEAMS OF THE RT TORQUE BOX AT FS 1273. THESE AREAS OF THE TORQUE BOX ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE TH
- [SDR DL72W960119](https://openairdocs.org/sdr/DL72W960119.md): Angle · cracked · Jan 17, 1996 · N292WA · Boeing 727247 · Leading Edge Devices
  > FOUND ON A1 LETTER CHECK, TWO.5 INCH CRACKS AT NR 2 L/E SLAT COVE SKIN ANGLE, BELOW TIA DUCT. REPAIRED PER MM 57-50-0.
- [SDR DL72W953096](https://openairdocs.org/sdr/DL72W953096.md): Stringer · corroded · Jul 14, 1995 · N292WA · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > STRINGER 27L CORRODED AT WIRE SUPPORT STA 570. REMOVED CORRODED AREA, FABRICATED REPAIR SPLICE AND FILLER. INSTALLED REPAIR PER SRM 53-10-3, FOUND AT HMV.
- [SDR DL72W953079](https://openairdocs.org/sdr/DL72W953079.md): Stringer · corroded · Jul 14, 1995 · N292WA · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > AT HMV, STR 27 L CORRODED AT WIRE SUPPORT STA 570. REMOVED CORRODED AREA, FABRICATED REPAIR SPLICE AND FILLER AS PER B-727 SRM 53-10-3.
- [SDR DL72W953032](https://openairdocs.org/sdr/DL72W953032.md): Rib · cracked · Jul 10, 1995 · N292WA · Boeing 727247 · Leading Edge Devices
  > NR 3 SLAT RIB CRACKED, I/B OF ACTUATOR ATTACH POINT CRACKED IN RADIUS AT LOWER AFT END OF RIB. INSTALLED DOUBLER PER MM 57-54-0 PG 819. FOUND AT HMV.
- [SDR DL72W953006](https://openairdocs.org/sdr/DL72W953006.md): Rib · cracked · Jul 8, 1995 · N292WA · Boeing 727247 · Leading Edge Devices
  > ITEM: NR 6 SLAT RIB CRACKED AT RIVET FWD FLANGE OF RIB NR 7. CORRECTION: REPAIRED PER S.R.M. 57-50-03, FIG 09. DAMAGE FOUND AT HMV.
- [SDR DL72W953001](https://openairdocs.org/sdr/DL72W953001.md): Skin · damaged · Jul 7, 1995 · N292WA · Boeing 727247 · Leading Edge Devices
  > AT HMV, FOUND NR 4 SLAT INNER ANTI-ICE SKIN BETWEEN NR 12, NR 13 RIBS HAS HOLE. FABRICATED AND INSTALLED DOUBLER PER MM 57-54-0, FIG 803A.
- [SDR DL72W953000](https://openairdocs.org/sdr/DL72W953000.md): Angle · cracked · Jul 7, 1995 · N292WA · Boeing 727247 · Leading Edge Devices
  > AT HMV, FOUND NR 4 SLAT ATTACH ANGLE ABOVE NR 13 RIB CRACKED. FABRICATED AND INSTALLED DOUBLER PER MM 57-54-0, PG 807.
- [SDR DL72W952965](https://openairdocs.org/sdr/DL72W952965.md): Skin · cracked · Jul 6, 1995 · N292WA · Boeing 727247 · Leading Edge Devices
  > NR 6 SLAT SKIN CRACKED AT TAB FOR INBD TRACK FAIRING ATTACH. INSTALLED REPAIR PER MM 57-54-0, PG 820/821. FOUND AT HMV.
- [SDR DL72W952934](https://openairdocs.org/sdr/DL72W952934.md): Bracket · cracked · Jul 5, 1995 · N292WA · Boeing 727247 · Leading Edge Devices
  > BRACKETS CRACKED, NR 2 KRUEGER FLAP ACTUATOR, O/B SUPPORT BRACKET AND I/B SUPPORT BRACKET. DYE CHECKED, FOUND NO DISCREPANCIES PER PS 900-6-301.
- [SDR DL72W952932](https://openairdocs.org/sdr/DL72W952932.md): Ribs · cracked · Jul 5, 1995 · N292WA · Boeing 727247 · Leading Edge Devices
  > AT HMV, FOUND NR 4 L/E SLAT WITH RIB NR 1, 10, 13, 15 CRACKED. REPAIRED CRACKED RIBS PER MM 57-54-0.
- [SDR DL72W952933](https://openairdocs.org/sdr/DL72W952933.md): Angle · cracked · Jul 4, 1995 · N292WA · Boeing 727247 · Leading Edge Devices
  > AT HMV, NR 4 SLAT ANGLE FOR CLOSEOUT PANEL CRACKED AT FWD LOWER EDGE AT RIB NR 12 AND NR 13. REPAIRED PER MM 57-54-0.
- [SDR DL72W952937](https://openairdocs.org/sdr/DL72W952937.md): Seat Track · corroded · Jul 2, 1995 · N292WA · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > AT HMV, SEAT TRACK CORRODED, FROM FS 1070-1110 RT IB TRACK RBL 24.5. REMOVED CORROSION PER SRM 51-10-06. REPLACED TRACK FROM FS 1070 TO 1110 PER MM 53-20-11, PG 806.
- [SDR DL72W952866](https://openairdocs.org/sdr/DL72W952866.md): Skin · hole · Jun 30, 1995 · N292WA · Boeing 727247 · Trailing Edge Flaps
  > AT HMV SHOP INSPECTION OF NR 1 F/F, WORN AREA FOUND 11 TO 12 INCHES FORM I/B END OF FLAP. ACCOMPLISHED REPAIRS PER SRM 57-50-4.
- [SDR DL72W952865](https://openairdocs.org/sdr/DL72W952865.md): Le Skin · worn · Jun 30, 1995 · N292WA · Boeing 727247 · Trailing Edge Flaps
  > AT HMV SHOP INSPECTION, NR 1 FOREFLAP FOUND WITH A HOLE IN THE L/E 10.5 INCHES FROM I/B END. REPAIRED PER SRM 57-50-4.
- [SDR DL72W952918](https://openairdocs.org/sdr/DL72W952918.md): Frame · misdrilled · Jun 29, 1995 · N292WA · Boeing 727247 · Fuselage Main, Frame
  > DURING HMV, EDGE DISTANCE COULD NOT BE MAINTAINED ON ONE OF THE FASTENER HOLES THROUGH THE FLOORBEAM UPPER CHORD AT FS 761 ON RT AND LT SIDES. FOUND DURING ACCOMPLISHMENT OF EO 4-61904-3AD. REPAIRED BY PLUGGING THE DISCREPANT HOLES AND CONTINUED EO 61904-3AD
- [SDR DL72W952890](https://openairdocs.org/sdr/DL72W952890.md): Seat Track · corroded · Jun 29, 1995 · N292WA · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED STA 344 RT SIDE O/B, C53-224-03. REPLACED SEAT TRACK O/B RT SIDE FROM 344 TO 360 PER SRM 53-20-11, FOUND AT HMV.
- [SDR DL72W952936](https://openairdocs.org/sdr/DL72W952936.md): Stringer · corroded · Jun 25, 1995 · N292WA · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > AT HMV, STR 27L CORRODED AT STA 720F PLUS 10. REPAIRED PER SRM 53-10-3.
- [SDR DL72W952898](https://openairdocs.org/sdr/DL72W952898.md): Support · damaged · Jun 25, 1995 · N292WA · Boeing 727247 · Wing Miscellaneous Structure
  > LT STA 913 UPLOCK SUPPORT FRAME HAS EXISTING TEMP REPAIR. INSTALLED REPAIR PER MM 53-11-0.
- [SDR DL72W952825](https://openairdocs.org/sdr/DL72W952825.md): Bushing · worn · Jun 25, 1995 · N292WA · Boeing 727247 · Trailing Edge Flaps
  > AT HMV, BUSHINGS WORN IN MLG DOOR LUG ON FWD END OF NR 5 FLAP TRACK. REPAIRED PER MM 57-43-0.
- [SDR DL72W952894](https://openairdocs.org/sdr/DL72W952894.md): Floorbeam · corroded · Jun 24, 1995 · N292WA · Boeing 727247 · Fuselage Main, Floor Beam
  > AT HMV, FOUND FS 1090 CABIN FLOORBEAM CORRODED AT RBL 45. ACCOMPLISHED REPAIRS PER SRM 53-10-8.

Next page: https://openairdocs.org/deregistered/N292WA-2010-07-20/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 = 'N292WA' AND deregistration_id = 'N292WA-2010-07-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N292WA-2010-07-20/reports

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