# Service difficulty reports: N256AY, cancelled Feb 5, 2022

A list on [N256AY, cancelled Feb 5, 2022](https://openairdocs.org/deregistered/N256AY-2022-02-05.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 3 · 121 reports

- [SDR USAA2014122400005](https://openairdocs.org/sdr/USAA2014122400005.md): Pump · leaking · Dec 22, 2014 · N256AY · Boeing 7672B7 · Turbine Engine Oil System
  > ENROUTE, RT ENGINE OIL PRESSURE DROPPED TO 13 PSI, WITH OIL QTY LOSS. SHUTDOWN THE RT ENGINE. LANDED WITHOUT FURTHER INCIDENT. REPLACED THE NR 2 ENGINE LUBE PUMP DUE TO DAMAGED THREADS ON THE TGB INLET SCREEN. REPLACED THE SCAVENGE OIL FILTER. CHECKED TH
- [SDR USAA2014062300013](https://openairdocs.org/sdr/USAA2014062300013.md): Handle · loose · Jun 21, 2014 · N256AY · Boeing 7672B7 · Passenger/Crew Doors
  > FWD ENTRY DOOR WOULD NOT ARM & DIFFICULT TO CLOSE. MX FOUND L1 DOOR ARMING HANDLE LOOSE. SECURED HANDLE. PERFORMED SATISFACTORY OPERATIONAL TEST OF L1 DOOR OPENING & CLOSING FUNCTIONS & SLIDE ARMING & DISARMING FUNCTIONS. ACFT OK FOR SERVICE.
- [SDR USAA2014042100004](https://openairdocs.org/sdr/USAA2014042100004.md): Power Supply · inoperative · Apr 17, 2014 · N256AY · Boeing 7672B7 · Emergency Lighting
  > CLT L1 & L2 DOOR EXIT & THRESHOLD LIGHTS WOULD NOT TEST. REPLACED M1208 POWER SUPPLY.
- [SDR USAA2013122700003](https://openairdocs.org/sdr/USAA2013122700003.md): Control Panel · faulty · Dec 26, 2013 · N256AY · Boeing 7672B7 · Cabin Pressure Control System
  > FLT 751 ENROUTE, RECEIVED FWD EQ OVERHEAT MESSAGE FOLLOWED BY UNCONTROLLABLE CABIN AIR PRESSURE. DECLARED AN EMERGENCY & PERFORMED A RAPID DESCENT TO 10,000 FT. RETURNED TO DEPARTURE & LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE CABIN PRESSURE SELECTO
- [SDR USAA2013121200001](https://openairdocs.org/sdr/USAA2013121200001.md): Slide · unsecure · Dec 12, 2013 · N256AY · Boeing 7672B7 · Escape Slide
  > C1 CHECK, RT OFF WING ESCAPE SLIDE ASSEMBLY UNLACED, SLIDE NOT SECURED. REPLACED RT ESCAPE SLIDE ASSEMBLY & INSTALLED IAW B767 AMM 25-65-05-424-056.
- [SDR USAA2013112200005](https://openairdocs.org/sdr/USAA2013112200005.md): Aileron · delaminated · Nov 18, 2013 · N256AY · Boeing 7672B7 · Ailerons
  > C1 CHECK DELAMINATION ON RT AILERON AT APPROXIMATELY 75 INCHES OTBD OF INBD END & 13.5 INCHES FWD OF AFT TE. REPLACED RT AILERON IAW JOB CARD 12L56027004.
- [SDR USAA2013111400009](https://openairdocs.org/sdr/USAA2013111400009.md): Skin · delaminated · Nov 13, 2013 · N256AY · Boeing 7672B7ER · Trailing Edge Flaps
  > DURING C1 CHECK, DELAMINATION WAS FOUND ON RT OTBD AFT FLAP APPROX 85 INCHES OTBD FROM INBD END LOWER SURFACE & 13.5 INCHES FORWARD OF T/E. REPAIRED RT AFT FLAP IAW SRM 57-53-01-2R-1.
- [SDR USAA2013111400008](https://openairdocs.org/sdr/USAA2013111400008.md): Skin · delaminated · Nov 10, 2013 · N256AY · Boeing 7672B7ER · Trailing Edge Flaps
  > DURING C1 CHECK, DELAMINATION FOUND ON RT AFT FLAP APPROX 14 INCHES FROM INBD END & 12 INCHES FROM T/E. REPAIRED RT AFT FLAP IAW SRM 51-70-10.
- [SDR USAA2013110800007](https://openairdocs.org/sdr/USAA2013110800007.md): Stiffener · cracked · Nov 6, 2013 · N256AY · Boeing 7672B7ER · Fuselage Miscellaneous Structure
  > DURING C1 CHECK, CRACK FOUND IN VERTICAL STIFFNER OF NOSE WHEEL WELL AT BS 287, WL 172, LBL 25. REPAIRED VERTICAL STIFFENER OF NOSE WHEEL WELL AT BS287, WL172, LBL25 IAW SRM 51-70-12 & EA 130449.
- [SDR USAA2013091600008](https://openairdocs.org/sdr/USAA2013091600008.md): Sign · unsecure · Sep 15, 2013 · N256AY · Boeing 7672B7ER · Emergency Lighting
  > EXIT SIGN OVER F/A J/S AT 2L DOOR IS OFF. R & R 2L EXIT SIGN.
- [SDR USAA2013091600006](https://openairdocs.org/sdr/USAA2013091600006.md): Cover · unsecure · Sep 14, 2013 · N256AY · Boeing 7672B7 · Emergency Lighting
  > EXIT SIGN COVER 2L JUMPSEAT FELL OUT. COVER REINSTALLED; OPC SATISF.
- [SDR USAA2013090900001](https://openairdocs.org/sdr/USAA2013090900001.md): Cable · shorted · Sep 7, 2013 · N256AY · Boeing 7672B7ER · Equipment/Furnishings Wiring
  > ENROUTE, ACFT RT AFT GALLEY A-302, CIRCUIT BREAKER TRIPPED. TRIED ONE RESET, STARTED SMOKING. PULLED CIRCUIT BREAKER AND UNPLUGGED CART. R & R AFT GALLEY CART CABLE. OP'S CHECED GOOD. NO OTHER DEFECTS NOTED.
- [SDR USAA2013072300001](https://openairdocs.org/sdr/USAA2013072300001.md): Cover · dislodged · Jul 21, 2013 · N256AY · Boeing 7672B7ER · Emergency Lighting
  > EXIT SIGN OVERWING EXIT ACFT LT COVER FELL OFF DURING TAKEOFF ROLL STRIKING PASSENGER IN SEAT 12A. MX SECURED EXIT SIGN OVERWING AS REQUIRED.
- [SDR USAA2013070300003](https://openairdocs.org/sdr/USAA2013070300003.md): Service Cart · faulty · Jul 1, 2013 · N256AY · Boeing 7672B7 · Buffet/Galleys
  > EN-ROUTE, THE GALLEY FOOD HEATING UNIT IN THE AFT GALLEY MELTED THE PLASTIC FOOD TRAYS AND EMITTED AN ODOR. THEY WERE NEW FOOD TRAYS. MX EXCHANGED ALL HEATING UNITS AND VISUALLY CHECKED ALL CORDS. NO DAMAGE FOUND.
- [SDR USAA2013050600002](https://openairdocs.org/sdr/USAA2013050600002.md): Battery · discharged · May 4, 2013 · N256AY · Boeing 7672B7ER · Emergency Equipment
  > PHL - FLASHLIGHT AT FWD F/A STATION BATTERY DEAD. REPLACED BATTERY.
- [SDR USAA2013042300002](https://openairdocs.org/sdr/USAA2013042300002.md): Sign · missing · Apr 21, 2013 · N256AY · Boeing 7672B7ER · Emergency Lighting
  > PHL - EXIT SIGN IN CEILING A/C RT AFT OF 1ST CLASS MISSING. RE-SECURED SIGN.
- [SDR USAA2013031900002](https://openairdocs.org/sdr/USAA2013031900002.md): Check Valve · failed · Mar 16, 2013 · N256AY · Boeing 7672B7ER · Engine (Turbine/Turboprop)
  > FLT 1628 ENROUTE, NR 2 ENGINE FLAMED OUT DURING REVERSE SELECTION ON LANDING. THE FLIGHT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MX REPLACED THE NR 2 ENGINE MEC AND FUEL PUMP, PERFORMED THE NR 2 ENGINE VSV ADJUSTMENT, AND CLEARED THE CDP AND CBP WATER
- [SDR USAA2013030600010](https://openairdocs.org/sdr/USAA2013030600010.md): Slide Raft · malfunctioned · Mar 6, 2013 · N256AY · Boeing 7672B7ER · Escape Slide
  > DURING ESCAPE SLIDE/RAFT OPS CHECK, TWO FWD SLIDE/RAFTS FAILED TO INFLATE PROPERLY. SLIDE DID NOT UNFOLD. CENTER WEBBING ATTACH POINT (BELOW GIRT) DID NOT BREAK AWAY. MAINTENANCE MANUALLY CUT WEBBING TO UNFOLD SLIDE. MAINTENANCE REPLACED THE ESCAPE SLIDE/R
- [SDR USAA2013012800001](https://openairdocs.org/sdr/USAA2013012800001.md): Reheater · contaminated · Jan 26, 2013 · N256AY · Boeing 7672B7ER · Cabin Cooling System
  > FLT 9465 TEST FLIGHT. FL 360, IN CRUISE. CABIN AND COCKPIT SMOKE NOTED. CREW DONNED O2 MASKS AND ENDED TEST FLIGHT. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT PACK REHEATER DUE TO CONTAMINATION.
- [SDR USAA2013012200005](https://openairdocs.org/sdr/USAA2013012200005.md): Power Unit · broken · Jan 18, 2013 · N256AY · Boeing 7672B7ER · Emergency Equipment
  > C4 CHECK - AFT CRT LEFT FLASHLIGHT POWER UNIT HAS A BROKEN WIRE. REPLACED AFT CRT LEFT FLASHLIGHT POWER UNIT IAW DME CORPORATION CMM 25-60-02.
- [SDR USAA2013012200004](https://openairdocs.org/sdr/USAA2013012200004.md): Sign · broken · Jan 17, 2013 · N256AY · Boeing 7672B7ER · Emergency Lighting
  > C4 CHECK - L2 DOOR LINER EXIT SIGN "L333" HAS BROKEN LIGHT COVER. REPLACED L-2 DOOR LINER EXIT SIGN "L333" & OPS CHECKS GOOD IAW B767 AMM 33-51-022-029 & 33-51-01-402-030.
- [SDR USAA2013011800010](https://openairdocs.org/sdr/USAA2013011800010.md): Light · broken · Jan 17, 2013 · N256AY · Boeing 7672B7ER · Emergency Lighting
  > C4 CHECK - WORN & BROKEN FORWARD & AFT GALLEY MAT EMERGENCY PATH LIGHT REQUIRES REPLACEMENT. REPLACED FORWARD & AFT GALLEY MAT EMERGENCY PATH LIGHT IAW DRAWING 12P25D0301.
- [SDR USAA2013011600005](https://openairdocs.org/sdr/USAA2013011600005.md): Light · cracked · Jan 14, 2013 · N256AY · Boeing 7672B7ER · Emergency Lighting
  > C4 CHECK - RIGHT CEILING PANEL 11 EMERGENCY LIGHT ASSY IS BROKEN. REPLACED RIGHT CEILING PANEL 11 EMERGENCY LIGHT ASSY (AISLE LIGHT). OPS CHECK GOOD IAW B767 AMM 33-51-05-002-016 & 33-51-05-402-024.
- [SDR USAA2013011500004](https://openairdocs.org/sdr/USAA2013011500004.md): Flap · damaged · Dec 29, 2012 · N256AY · Boeing 7672B7ER · Trailing Edge Flaps
  > C4 CHECK - FIBER DAMAGE ON RIGHT OUTBOARD FLAP LOWER TRAILING EDGE BETWEEN DTEF265.88 TO DTEF267.88. REPAIRED RIGHT OUTBOARD FLAP LOWER TRAILING EDGE BETWEEN DTEF265.88 TO DTEF267.88 IAW B767 SRM 51-70-06-0G, REPAIR A, FIG. 9.
- [SDR USAA2013010300027](https://openairdocs.org/sdr/USAA2013010300027.md): Floorbeam · corroded · Dec 27, 2012 · N256AY · Boeing 7672B7ER · Fuselage Main, Floor Beam
  > C4 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM AT BS 303, LBL 13. REPAIRED FLOORBEAM AT BS 303, LBL 13 IAW B767 SRM 53-00-51-2R-1 FIG 201.
- [SDR USAA2012122800018](https://openairdocs.org/sdr/USAA2012122800018.md): Floorbeam · corroded · Dec 20, 2012 · N256AY · Boeing 7672B7ER · Fuselage Main, Floor Beam
  > C4 CHECK - LEVEL 2 FILIFORM CORROSION ON FLOORBEAM AT BS 1518, LBL 30. REPAIRED FLOORBEAM AT BS 1518, LBL 30 IAW B767 SRM 53-00-51-2R-1 FIG 201.
- [SDR USAA2013012500014](https://openairdocs.org/sdr/USAA2013012500014.md): Channel · cracked · Dec 19, 2012 · N256AY · Boeing 7672B7ER · Fuselage Miscellaneous Structure
  > C4 CHECK - CRACK ON FLOOR SUPPORT CHANNEL BETWEEN BS 347 & BS 357, RBL 34. REPLACED FLOOR SUPPORT CHANNEL BETWEEN BS 347 & BS 357, RBL 34 IAW B767 SRM 51-40-02-0G, PAR 7, FIG 8 & 12.
- [SDR USAA2013011500005](https://openairdocs.org/sdr/USAA2013011500005.md): Floorbeam · corroded · Dec 19, 2012 · N256AY · Boeing 7672B7ER · Fuselage Main, Floor Beam
  > C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS 347, RBL 46.25. REPAIRED FLOORBEAM T-CAP AT BS 347, RBL 46.25 IAW B767 SRM 53-00-51-2R-1, FIG 201.
- [SDR USAA2013012500015](https://openairdocs.org/sdr/USAA2013012500015.md): Attach Fitting · cracked · Dec 18, 2012 · N256AY · Boeing 7672B7ER · Fuselage Miscellaneous Structure
  > C4 CHECK - CRACK ON FRAME ATTACH CLIP AT BS 1562, S33L. REPLACED FRAME ATTACH CLIP AT BS 1562, S33L IAW BOEING DRAWING 216T1014.
- [SDR USAA2013012500013](https://openairdocs.org/sdr/USAA2013012500013.md): Floor Support · cracked · Dec 18, 2012 · N256AY · Boeing 7672B7ER · Fuselage Miscellaneous Structure
  > C4 CHECK - CRACK ON FLOOR SUPPORT WEB UPPER CHORD AT B S1412, LBL 40. REPLACED FLOOR SUPPORT WEB UPPER CHORD AT BS 1412, LBL 40 IAW B767 SRM 51-40-02-0G, PAR. 4, FIG 3 & 12.
- [SDR USAA2012121800026](https://openairdocs.org/sdr/USAA2012121800026.md): Floorbeam · corroded · Dec 14, 2012 · N256AY · Boeing 7672B7ER · Fuselage Main, Floor Beam
  > C4 CHECK - CORROSION ON FLOORBEAM REPAIR STRAP AT BS 347, RBL 68. REPLACED FLOORBEAM REPAIR STRAP AT BS 347, RBL 68 IAW B767 SRM 53-00-51-2R-2 FIG 201.
- [SDR USAA2012121300006](https://openairdocs.org/sdr/USAA2012121300006.md): Placard · missing · Dec 9, 2012 · N256AY · Boeing 7672B7ER · Placards and Markings
  > C4 CHECK - LEFT AND RIGHT OVERWING HATCHES MISSING PLACARD. INSTALLED LEFT AND RIGHT OUTER WING HATCHES MISSING PLACARD IAW B767 AMM 20-10-13-964-001.
- [SDR USAA2013010300024](https://openairdocs.org/sdr/USAA2013010300024.md): Shear Web · cracked · Dec 7, 2012 · N256AY · Boeing 7672B7ER · Nacelle/Pylon Miscellaneous Structure
  > C4 CHECK - CRACK IN LEFT PYLON FORWARD SPAR UPPER SHEAR WEB AT NAC STA 227, LBL 5. REPAIRED LEFT PYLON FORWARD SPAR UPPER SHEAR WEB AT NAC STA 227, LBL 5 IAW EO 5403T119, PG III-9, STEP G & E.
- [SDR USAA2013011500003](https://openairdocs.org/sdr/USAA2013011500003.md): Floor Support · damaged · Dec 4, 2012 · N256AY · Boeing 7672B7ER · Fuselage Miscellaneous Structure
  > C4 CHECK - ELONGATED HOLES ON CABIN FLOOR STRUCTURE SUPPORT WEB AT BS 1412, LBL 40. REPLACED CABIN FLOOR STRUCTURE SUPPORT WEB AT BS 1412, LBL 40 IAW B767 SRM 51-40-02-0G, FIG 12.
- [SDR USAA2012120700005](https://openairdocs.org/sdr/USAA2012120700005.md): Fastener · damaged · Dec 4, 2012 · N256AY · Boeing 7672B7ER · Emergency Equipment
  > C4 CHECK - RIGHT OFF WING SLIDE LATCH ACTUATOR HAS DAMAGED HARDWARE. REMOVED AND REPLACED HARDWARE IAW B767 AMM 20-11-00-427-003. USED TW 1111113012
- [SDR USAA2012120700004](https://openairdocs.org/sdr/USAA2012120700004.md): Fastener · damaged · Dec 4, 2012 · N256AY · Boeing 7672B7ER · Emergency Equipment
  > C4 CHECK - RIGHT OFF WING SLIDE INTEGRATOR HAS DAMAGED HARDWARE. REMOVED AND REPLACED HARDWARE IAW B767 AMM 20-11-00-422-003. USED TW 1111113012.
- [SDR USAA2012120600005](https://openairdocs.org/sdr/USAA2012120600005.md): Spring · weak · Dec 4, 2012 · N256AY · Boeing 7672B7ER · Passenger/Crew Doors
  > C4 CHECK, L-2 DOOR DEPLOYMENT BAR GAS SPRING WEAK. REMOVED AND REPLACED L-2 DOOR DEPLOYMENT BAR GAS SPRING IAW B767 AMM 25-66-03-004-053 AND 25-66-03-404-067.
- [SDR USAA2012120600004](https://openairdocs.org/sdr/USAA2012120600004.md): Spring · weak · Dec 4, 2012 · N256AY · Boeing 7672B7ER · Passenger/Crew Doors
  > C4 CHECK, L-1 DOOR DEPLOYMENT BAR GAS SPRING WEAK. REMOVED AND REPLACED L-1 DOOR DEPLOYMENT BAR GAS SPRING IAW B767AMM 25-66-03-004-053 AND 25-66-03-404-067.
- [SDR USAA2013011500010](https://openairdocs.org/sdr/USAA2013011500010.md): Skin · corroded · Dec 1, 2012 · N256AY · Boeing 7672B7ER · Fuselage Main, Plate/Skin
  > C4 CHECK - CORROSION FUSELAGE SKIN AT BS 959, LBL 94. REPAIRED FUSELAGE SKIN AT BS 959, LBL 94 IAW EA 131979.
- [SDR USAA2013011500009](https://openairdocs.org/sdr/USAA2013011500009.md): Skin · corroded · Dec 1, 2012 · N256AY · Boeing 7672B7ER · Fuselage Main, Plate/Skin
  > C4 CHECK - CORROSION FUSELAGE SKIN AT BS 955, RBL 92. REPAIRED FUSELAGE SKIN AT BS 955, RBL 92 IAW EA 131979.
- [SDR USAA2013010300025](https://openairdocs.org/sdr/USAA2013010300025.md): Frame · cracked · Dec 1, 2012 · N256AY · Boeing 7672B7ER · Nacelle/Pylon, Frame/Spar/Rib
  > C4 CHECK - CRACK IN LEFT PYLON FRAME AT NAC STA 285.30, WL 148.0, LBL 12. REPAIRED LEFT PYLON FRAME AT NAC STA 285.30, WL 148.0, LBL 12 IAW B767 SRM 51-40-02-0G FIG 12.
- [SDR USAA2013012500016](https://openairdocs.org/sdr/USAA2013012500016.md): Structure · corroded · Nov 30, 2012 · N256AY · Boeing 7672B7ER · Fuselage Miscellaneous Structure
  > C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON CENTER WING UPPER SKIN AT BS 955, RBL 4. REPAIRED CENTER WING UPPER SKIN AT BS 955, RBL4 IAW EA 504597A.
- [SDR USAA2013010800024](https://openairdocs.org/sdr/USAA2013010800024.md): Floorbeam · corroded · Nov 29, 2012 · N256AY · Boeing 7672B7ER · Fuselage Main, Floor Beam
  > C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT BS 1480, LBL 44. REPAIRED FLOORBEAM AT BS 1480, LBL 44 IAW B767 SRM 53-00-51-2R-1 FIG 201.
- [SDR USAA2013010300026](https://openairdocs.org/sdr/USAA2013010300026.md): Attach Angle · cracked · Nov 29, 2012 · N256AY · Boeing 7672B7ER · Fuselage Miscellaneous Structure
  > C4 CHECK - CRACK ON CABIN FLOOR SUPPORT WEB UPPER ATTACH ANGLE CHORD BETWEEN BS 1087 TO BS 1109, LBL 39. REPLACED CABIN FLOOR SUPPORT WEB UPPER ATTACH ANGLE CHORD BETWEEN BS 1087 TO BS 1109, LBL 39 IAW B767 SRM 51-40-02-0G FIG 3.
- [SDR USAA2013011500006](https://openairdocs.org/sdr/USAA2013011500006.md): Seat Track · corroded · Nov 28, 2012 · N256AY · Boeing 7672B7ER · Fuselage, Seat/Cargo Attach Fittings
  > C4 CHECK - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN BS 1263 TO BS 1285, RBL 88.5. REPLACED SEAT TRACK BETWEEN BS 1263 TO BS 1285, RBL 88.5 IAW B767 SRM 51-40-02-0G, FIG 16.
- [SDR USAA2012121800023](https://openairdocs.org/sdr/USAA2012121800023.md): Structure · cracked · Nov 28, 2012 · N256AY · Boeing 7672B7ER · Fuselage Miscellaneous Structure
  > C3 CHECK - CRACK ON CHORD AT BS 1382, RBL 39. REPLACED CHORD AT BS 1382, RBL 39 IAW B767 SRM 51-40-02-0G FIG 3.
- [SDR USAA2012122100022](https://openairdocs.org/sdr/USAA2012122100022.md): Structure · cracked · Nov 27, 2012 · N256AY · Boeing 7672B7ER · Fuselage Miscellaneous Structure
  > C4 CHECK - CRACKS ON CABIN FLOOR STRUCTURE SUPPORT WEB UPPER ATTACH ANGLE CHORD BETWEEN BS1241 TO BS 1262, RBL 39. REPLACED CABIN FLOOR STRUCTURE SUPPORT WEB UPPER ATTACH ANGLE CHORD BETWEEN BS 1241 TO BS 1262, RBL 39 IAW B767 SRM 51-40-02-0G FIG 3, 8, 12.
- [SDR USAA2013012500012](https://openairdocs.org/sdr/USAA2013012500012.md): Floor Support · cracked · Nov 27, 2012 · N256AY · Boeing 7672B7ER · Fuselage Miscellaneous Structure
  > C4 CHECK - CRACK ON FLOOR SUPPORT WEB UPPER CHORD BETWEEN BS 1087 TO BS 1109, RBL 39. REPLACED FLOOR SUPPORT WEB UPPER CHORD BETWEEN BS 1087 TO BS 1109, RBL 39 IAW B767 SRM 51-40-02-0G, FIGS 3, 8 & 12.
- [SDR USAA2013011500008](https://openairdocs.org/sdr/USAA2013011500008.md): Failsafe · cracked · Nov 19, 2012 · N256AY · Boeing 7672B7ER · Fuselage Main, Frame
  > C4 CHECK - CRACK ON RIGHT FUSELAGE FAIL SAFE STRAP AT BS 959, RBL 92. REPAIRED RIGHT FUSELAGE FAIL SAFE STRAP AT BS 959, RBL 92 IAW EA 131979.
- [SDR USAA2013011500007](https://openairdocs.org/sdr/USAA2013011500007.md): Failsafe · cracked · Nov 19, 2012 · N256AY · Boeing 7672B7ER · Fuselage Main, Frame
  > C4 CHECK - CRACK ON LEFT FUSELAGE FAIL SAFE STRAP AT BS 959, LBL92. REPAIRED LEFT FUSELAGE FAIL SAFE STRAP AT BS 959, LBL92 IAW EA 131979.

Next page: https://openairdocs.org/deregistered/N256AY-2022-02-05/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 = 'N256AY' AND deregistration_id = 'N256AY-2022-02-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N256AY-2022-02-05/reports

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