# Service difficulty reports: N10791, cancelled Dec 5, 2001

A list on [N10791, cancelled Dec 5, 2001](https://openairdocs.org/deregistered/N10791-2001-12-05.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 2 · 78 reports

- [SDR CALA9901477](https://openairdocs.org/sdr/CALA9901477.md): Light · inop · Nov 8, 1999 · N10791 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND INTERIOR OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 22. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD.
- [SDR CALA9901073](https://openairdocs.org/sdr/CALA9901073.md): Floorbeam · corroded · Aug 19, 1999 · N10791 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND MAIN DECK FLOORBEAM IN AFT CARGO COMPARTMENT CORRODED AT STA 1130 FROM BL 0 TO RBL 30. REPAIRED IAW SRM 53-10-8 AND ECRA 5310-03898.
- [SDR CALA9900621](https://openairdocs.org/sdr/CALA9900621.md): Accessory Unit · inoperative · Jun 2, 1999 · N10791 · Boeing 727232 · Landing Gear Position and Warning
  > WHEN GEAR WAS RETRACTED AFTER DEPARTURE A LOUD THUMP WAS HEARD WHEN NOSE GEAR RETRACTED. A LIGHT TEST WAS DONE AND THE NOSE GEAR GREEN LIGHT DID NOT COME ON. PRESS TO TEST AND NEW BULBS HAD NO EFFECT. FLIGHT MANUAL PROCEDURE WAS ACCOMPLISHED. THE LIGHT TES
- [SDR CALA9900024](https://openairdocs.org/sdr/CALA9900024.md): Stator · migrated · Jan 16, 1999 · N10791 · Boeing 727232 · Turbine Engine Compressor Section
  > ENGINE NUMBER THREE FAILED ON CLIMB-OUT. CONSTANT VIBRATION, OVER TEMP, ENGINE SHUT DOWN IN FLIGHT. AIRCRAFT RETURNED TO LAS. ENGINE AND DAMAGED COWLING REPLACED AND AIRCRAFT RETURNED TO SERVICE. PRELIMINARY ENGINE INSPECTION REVEALED A FAILURE IN THE HIGH
- [SDR CALA9800812](https://openairdocs.org/sdr/CALA9800812.md): Battery · discharged · May 7, 1998 · N10791 · Boeing 727232 · Emergency Lighting
  > MAIN CABIN O/H EMERGENCY LIGHT FLICKERING. RECHARGED BATTERY PACK PER MM 33-50-0.
- [SDR CALA9800747](https://openairdocs.org/sdr/CALA9800747.md): Frame · cracked · May 3, 1998 · N10791 · Boeing 727232 · Fuselage Main, Frame
  > TOP FLANGE AT FRAME 520 HAS.5 INCH CRACK ABOVE STR 26R. STOP DRILLED CRACK PER SRM 51-10-1. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-6. HEAT TREAT PER BAC 5602.
- [SDR CALA9800746](https://openairdocs.org/sdr/CALA9800746.md): Oxy Contl Unit · failed · May 3, 1998 · N10791 · Boeing 727232 · Passenger Oxygen System
  > FWD OXYGEN PASSENGER DROP FAILED FUNCTIONAL TEST. REPLACED OXYGEN CONTROL UNIT AND PERFORMED PNEUMATIC OXYGEN DROP PER MM 35-21-00.
- [SDR CALA9800745](https://openairdocs.org/sdr/CALA9800745.md): Web · cracked · May 3, 1998 · N10791 · Boeing 727232 · Vertical Stabilizer
  > VERT STAB INNER COMPARTMENT NR 1 CANTED STATION 1303 HAS CRACK (2.5) AT RT LOWER CORNER. ALSO, CRACK (1) AT RT UPPER CORNER. STOP DRILLED CRACKS, FABRICATED AND INSTALLED DOUBLERS PER SRM 51-40-2.
- [SDR CALA9800744](https://openairdocs.org/sdr/CALA9800744.md): Stringer · cracked · May 3, 1998 · N10791 · Boeing 727232 · Vertical Stabilizer
  > VERT STAB INNER COMPARTMENT NR 7 STRINGER NR 2 AND NR 3 CRACKED (2) AT ATTACH BOLT. REPAIRED NR 7 RT STRINGER NR 2 AND NR 3 ON VERTICAL STAB PER SRM 55-30-4.
- [SDR CALA9800743](https://openairdocs.org/sdr/CALA9800743.md): Jamb · cracked · May 3, 1998 · N10791 · Boeing 727232 · Fuselage Miscellaneous Structure
  > C-1 DOOR JAMB BENT/TORN AT TWO PLACES. REMOVED AND REPLACED DOOR JAMB AS REQUIRED PER SRM 51-10-1.
- [SDR CALA9800742](https://openairdocs.org/sdr/CALA9800742.md): Flange · cracked · May 3, 1998 · N10791 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TOP FLANGE RADIUS FS 700 ABOVE 24 L HAS 1.5 INCH CRACK. STOP DRILLED, FABRICATED DOUBLER AND INSTALLED PER SRM 51-30-2 AND 51-40-3.
- [SDR CALA9800741](https://openairdocs.org/sdr/CALA9800741.md): Wire · broken · May 3, 1998 · N10791 · Boeing 727232 · Light System Wiring
  > LT EXIT LIGHT INOP OVER EXIT IN CABIN. REPAIRED BROKEN WIRE AT EXIT IDENTIFIER, OPS CHECK PER 33-50-00.
- [SDR CALA9800740](https://openairdocs.org/sdr/CALA9800740.md): Flange · cracked · May 3, 1998 · N10791 · Boeing 727232 · Fuselage Main, Frame
  > A 1 INCH CRACK AT FRAME 500 TOP FLANGE RADIUS ABOVE 24 L. FABRICATED NEW DOUBLER AND INSTALLED IN ACCORDANCE WITH SRM 51-40-3. HEAT TREATED PER BAC 5602.
- [SDR CALA9800739](https://openairdocs.org/sdr/CALA9800739.md): Skin · corroded · May 3, 1998 · N10791 · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN IN FORWARD BAG BIN FS 695.700 AT RBL HAS SURFACE CORROSION. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-30-03.
- [SDR CALA9800738](https://openairdocs.org/sdr/CALA9800738.md): Wire · broken · May 3, 1998 · N10791 · Boeing 727232 · Light System Wiring
  > ESCAPE PATH LIGHTS INOP ROW 24 TO 29. REPAIRED BROKEN WIRE GOING TO SEATS PER MM 33-50-00.
- [SDR CALA9800701](https://openairdocs.org/sdr/CALA9800701.md): Support · cracked · Apr 24, 1998 · N10791 · Boeing 727232 · Vertical Stabilizer
  > INSPECTION FOUND A 2.5 CRACK IN VERTICAL STABILIZER STRINGER 4L SUPPORT WEB. THE SUPPORT WEB WAS REMOVED IAW SRM 51-30-2. A NEW SUPPORT WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
- [SDR CALA9800700](https://openairdocs.org/sdr/CALA9800700.md): Support · cracked · Apr 24, 1998 · N10791 · Boeing 727232 · Vertical Stabilizer
  > INSPECTION FOUND A 1 CRACK IN VERTICAL STABILIZER SUPPORT WEB AT STRINGER 3L AND STRINGER 3R. THE LT AND RT SUPPORT WEB WAS REMOVED. A NEW SUPPORT WEB WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
- [SDR CALA9800699](https://openairdocs.org/sdr/CALA9800699.md): Frame · cracked · Apr 24, 1998 · N10791 · Boeing 727232 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 CRACK IN UPPER FLANGE RADIUS OF FRAME 640, RBL 8, FORWARD BAGGAGE BIN. THE CRACKED AREA WAS CUT OUT IAW SRM 51-40-3. A DOUBLER AND FITTING WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, FIGURE 1, SHEET A, SRM 51-10-2, AND 51-30-2.
- [SDR CALA9800698](https://openairdocs.org/sdr/CALA9800698.md): Frame · cracked · Apr 24, 1998 · N10791 · Boeing 727232 · Fuselage Main, Frame
  > INSPECTION FOUND A.375 INCH CRACK WITH CORROSION IN FRAME 560 TO SKIN ATTACH FLANGE, BBL 0 TO LBL 6. THE CORRODED AREA OF FLANGE WAS CUT OFF IAW SRM 53-10-4. A NEW FLANGE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4.
- [SDR CALA9800697](https://openairdocs.org/sdr/CALA9800697.md): Stringer · corroded · Apr 24, 1998 · N10791 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 28L CORRODED AT STA 720D. THE CORRODED AREA OF STRINGER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 53-10-3.
- [SDR CALA9800472](https://openairdocs.org/sdr/CALA9800472.md): Hyd Pump · leaking · Mar 17, 1998 · N10791 · Boeing 727232 · Hydraulic Pump (Electric/Engine), Main
  > THE 'A' SYSTEM HYDRAULIC RESERVOIR QUANTITY WENT TO ZERO AND LOW PRESSURE LIGHTS ILLUMINATED WHILE EN ROUTE FROM MSY TO IAH. THE HYDRAULIC QUANTITY LOSS AND HYDRAULIC SYSTEM FAILURE CHECKLISTS WERE COMPLETED. THE LANDING GEAR WAS CRANKED DOWN AND THE FLAPS W
- [SDR CALA9701375](https://openairdocs.org/sdr/CALA9701375.md): Beam · cracked · Aug 31, 1997 · N10791 · Boeing 727232 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.365 INCH AND.625 INCH CRACK IN RT WING UPPER TRAILING EDGE AFT OF MLG SUPPORT BEAM AT UPPER INBOARD CORNER OF NR 8 SPOILER ACTUATOR LINKAGE CASTING, WS 232. THE CRACKS WERE ROUTED OUT. REPAIR STRAPS WERE FABRICATED AND INSTALLED IAW ECRA
- [SDR CALA9701372](https://openairdocs.org/sdr/CALA9701372.md): Doubler · corroded · Aug 26, 1997 · N10791 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION AND POPPED RIVETS IN REPAIR DOUBLER AT FS 680, STRINGER 28R - 28L. THE EXISTING DOUBLER WAS REMOVED AND THE CORRODED AREA WAS CUT OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3.
- [SDR CALA9701374](https://openairdocs.org/sdr/CALA9701374.md): Skin · punctured · Aug 25, 1997 · N10791 · Boeing 727232 · Leading Edge Devices
  > INSPECTION FOUND A.25 INCH DIAMETER HOLE IN SKIN AT UPPER LEADING EDGE OF NR 7 SLAT. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-50-3.
- [SDR CALA9701371](https://openairdocs.org/sdr/CALA9701371.md): Bracket · cracked · Aug 25, 1997 · N10791 · Boeing 727232 · Leading Edge Slat Actuator
  > INSPECTION FOUND A.5 CRACK IN UPPER AND LOWER RADIUS OF NR 5 KRUGER FLAP ACTUATOR SUPPORT BRACKET. A REPLACEMENT BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1.
- [SDR CALA9701369](https://openairdocs.org/sdr/CALA9701369.md): Skin · cracked · Aug 25, 1997 · N10791 · Boeing 727232 · Wing, Plate/Skin
  > INSPECTION FOUND A.375 INCH CRACK AT LEFT WING FIXED LEADING EDGE CUTOUT ABOVE NR 3 SLAT INBOARD TRACK. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, 51-30-2, AND 51-40-2.
- [SDR CALA9701373](https://openairdocs.org/sdr/CALA9701373.md): Skin · dented · Aug 24, 1997 · N10791 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND TWO DENTS IN RT FUSELAGE SKIN AT STA 380. THE DENTED AREA WAS CUT OUT. FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3.
- [SDR CALA9701370](https://openairdocs.org/sdr/CALA9701370.md): Bracket · cracked · Aug 24, 1997 · N10791 · Boeing 727232 · Leading Edge Slat Actuator
  > INSPECTION FOUND A.75 CRACK IN BRACKET AT INBOARD AND OUTBOARD SIDE WHERE LEFT WING NR 1 L/E FLAP ACTUATOR MOUNTS (I/B LOWER AND O/B UPPER). REPLACEMENT BRACKETS WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-10-2.
- [SDR CALA9700343](https://openairdocs.org/sdr/CALA9700343.md): Actuator · leaking · Mar 16, 1997 · N10791 · Boeing 727232 · Leading Edge Slat Actuator
  > AIRCRAFT LOST A-HYDRAULIC SYSTEM FLUID AFTER TAKEOFF. THE LOSS WAS ACCOMPANIED BY ILLUMINATION OF RUDDER SYSTEM A CAUTION LIGHT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 KREUGER FLAP ACTUATOR LEAKING. TH
- [SDR CALA9700125](https://openairdocs.org/sdr/CALA9700125.md): Hyd Pump · leaking · Jan 30, 1997 · N10791 · Boeing 727232 · Hydraulic Pump (Electric/Engine), Main
  > ACFT LOST THE A-HYDRAULIC SYSTEM FLUID QUANTITY ON APPROACH. THE FLUID LOSS WAS ACCOMPANIED BY THE PUMP LIGHT GOING ON AND OFF INTERMITTENTLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP LEAKING AT PUMP CASE
- [SDR CALA9601731](https://openairdocs.org/sdr/CALA9601731.md): Skin · damaged · Nov 19, 1996 · N10791 · Boeing 727232 · Trailing Edge Flaps
  > THE RT INBOARD TRAILING EDGE MID FLAP LOWER SKIN SUSTAINED DAMAGE WHEN THE RT MLG TIRE BLEW. THE MID FLAP WAS REPAIRED IAW ECRA 5750-02565.
- [SDR CALA9601378](https://openairdocs.org/sdr/CALA9601378.md): Gearbox · leaking · Oct 4, 1996 · N10791 · Boeing 727232 · Turbine Engine Accessory Drive
  > THE NR 3 ENGINE LOST OIL QUANTITY AFTER TAKEOFF. THE LOSS OF OIL WAS ACCOMPANIED BY LOSS OF OIL PRESSURE AND ILLUMINATION OF FORWARD PANEL LIGHT. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO SJU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR
- [SDR CALA9601303](https://openairdocs.org/sdr/CALA9601303.md): Duct · blown · Sep 11, 1996 · N10791 · Boeing 727232 · Pneumatic Distribution System
  > THE NR 2 ENGINE FAILED AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO SJU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE 13TH STAGE DUCT BLOWN. THE NR 2 ENGINE WILL BE REMOVED AND REPLACED.
- [SDR CALA9601146](https://openairdocs.org/sdr/CALA9601146.md): Airstairs · out of adjust · Aug 7, 1996 · N10791 · Boeing 727232 · Entrance Stairs
  > THE AFT AIRSTAIRS FELL DOWN WHILE TAXIING TO GATE AFTER LANDING AT IAH. THE AIRCRAFT WAS STOPPED AND THE STAIRS WERE SECURED. WHEN THE AIRSTAIRS WAS EXAMINED FOR DAMAGE ONLY A SKID MARK WAS FOUND ON THE SKID PLATE. THE AIRSTAIR WAS OPERATED SEVERAL TIMES.
- [SDR CALA9600970](https://openairdocs.org/sdr/CALA9600970.md): Actuator · leaking · Jul 6, 1996 · N10791 · Boeing 727232 · Leading Edge Slat Actuator
  > THE A-SYSTEM HYDRAULIC QUANTITY WAS LOST DURING CLIMBOUT. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 LEADING EDGE FLAP ACTUATOR LEAKING. THE ACTUATOR WAS REMOVED AND REPLACED. IN ADDITI
- [SDR CALA9600956](https://openairdocs.org/sdr/CALA9600956.md): Floorbeam · corroded · Jun 30, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND THE FLOORBEAM CORRODED AT STA 1130, RBL 34 DURING FLIGHT PHONE INSTALLATION. THE FLOORBEAM WAS REPAIRED IAW SRM 5310-03300.
- [SDR CALA9600913](https://openairdocs.org/sdr/CALA9600913.md): Shear Tie · corroded · Jun 10, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SHEAR TIE CORRODED AT STA 580 BETWEEN STRINGER 27R AND 28R. THE SHEAR TIE WAS REMOVED AND A NEW SHEAR TIE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 53-10-4, FIG 15 AND MM 51-20-2, 51-20-15.
- [SDR CALA9600901](https://openairdocs.org/sdr/CALA9600901.md): Stringer · corroded · Jun 5, 1996 · N10791 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 28R FLANGE CORRODED AT F.S. 685. THE CORRODED SECTION OF STRINGER WAS REMOVED. A NEW STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3.
- [SDR CALA9600936](https://openairdocs.org/sdr/CALA9600936.md): Stringer · corroded · Jun 2, 1996 · N10791 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 28R CORRODED AT STA 520 T0 540. THE CORRODED STRINGER SECTION WAS REMOVED. A NEW STRINGER AND SPLICE WERE FABRICATED AND INSTALLED IAW SRM 53-10-3 AND 51-30-2.
- [SDR CALA9600938](https://openairdocs.org/sdr/CALA9600938.md): Angle · corroded · May 29, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON SKIN ATTACH ANGLE AT STA 580, STRINGER 27L. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, 51-30-2 AND MM 51-20-11.
- [SDR CALA9600915](https://openairdocs.org/sdr/CALA9600915.md): Support · corroded · May 28, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND THE FORWARD CARGO COMPARTMENT FLOOR SUPPORT CORRODED AT STA 535, S28L TO S29L. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-6, 51-40-4, 51-10-2, 53-10-1 AND 51-30-2.
- [SDR CALA9600919](https://openairdocs.org/sdr/CALA9600919.md): Shear Tie · corroded · May 26, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SHEAR TIE CORRODED AT STA 265, S25R. A REPAIR WAS PERFORMED IAW SRM 53-10-4, 51-10-2, 51-30-2 AND MM 51-20-21.
- [SDR CALA9600914](https://openairdocs.org/sdr/CALA9600914.md): Skin · corroded · May 26, 1996 · N10791 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND SKIN LAP CORRODED AT STA 720D TO 720E, STRINGER 27R. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-30-2.
- [SDR CALA9600935](https://openairdocs.org/sdr/CALA9600935.md): Angle · corroded · May 25, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ATTACH ANGLE CORRODED AT STA 540, S29R. THE ATTACH ANGLE WAS REMOVED. A REPAIR PART WAS FABRICATED IAW SRM 53-10-4, 53-10-1 AND 51-20-4.
- [SDR CALA9600934](https://openairdocs.org/sdr/CALA9600934.md): Frame · corroded · May 25, 1996 · N10791 · Boeing 727232 · Fuselage Main, Frame
  > INSPECTION FOUND STA 540 FRAME ASSEMBLY CORRODED. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, PAGE 43.
- [SDR CALA9600902](https://openairdocs.org/sdr/CALA9600902.md): Angles · corroded · May 25, 1996 · N10791 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SKIN ATTACH ANGLES(2) AT BILGE, STA 580, BL ZERO CORRODED. ANGLE DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2, AND MM 51-20-0.
- [SDR CALA9600900](https://openairdocs.org/sdr/CALA9600900.md): Floor Beam · corroded · May 24, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT B.S. 1130, LBL 25. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-1, 53-10-8, AND MM 51-20-11.
- [SDR CALA9600923](https://openairdocs.org/sdr/CALA9600923.md): Floor Beam · corroded · May 23, 1996 · N10791 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, LBL 30. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-2, 51-30-4 AND MM 51-20-11.
- [SDR CALA9600912](https://openairdocs.org/sdr/CALA9600912.md): Web · cracked · May 23, 1996 · N10791 · Boeing 727232 · Vertical Stabilizer
  > INSPECTION FOUND A FOUR INCH CRACK IN STIFFENER WEB INSIDE VERTICAL FIN ABOVE S-DUCT AT STA 1348. THE CRACK WAS STOPPED DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, 51-30-2 AND MM 51-20-11.
- [SDR CALA9600909](https://openairdocs.org/sdr/CALA9600909.md): Skin · cracked · May 23, 1996 · N10791 · Boeing 727232 · Wing, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN RT WING LEADING EDGE SKIN FORWARD OF OUTBOARD SLAT CARRIAGE, NR 5 SLAT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 57-30-4, FIG 4 AND 9, MM 51-20-11.

Next page: https://openairdocs.org/deregistered/N10791-2001-12-05/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 = 'N10791' AND deregistration_id = 'N10791-2001-12-05'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N10791-2001-12-05/reports

---
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