# Service difficulty reports: N69742, cancelled Jun 1, 2017

A list on [N69742, cancelled Jun 1, 2017](https://openairdocs.org/deregistered/N69742-2017-06-01.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR 20001103SH002](https://openairdocs.org/sdr/20001103SH002.md): Fitting · corroded · Jun 10, 2000 · N69742 · Boeing 727224 · Fuselage Main, Bulkhead
  > LEFT WING - BODY BULKHEAD FITTING STA 870 WITH PITTING CORROSION AT AFT FACE SURFACE AND INSIDE OF BORE. (X)
- [SDR 20001102SH040](https://openairdocs.org/sdr/20001102SH040.md): Skin · corroded · Jun 10, 2000 · N69742 · Boeing 727224 · Fuselage Main, Plate/Skin
  > CORROSION AT LEFT SCAN LIGHT CUT-OUT AREA INSIDE FUSELAGE ON SKIN STA 720B - STA 720C, STR 14R - STR 16R. (X)
- [SDR 20001102SH039](https://openairdocs.org/sdr/20001102SH039.md): Vent Line · chafed · Jun 10, 2000 · N69742 · Boeing 727224 · Fuel Storage
  > LEFT WING FUEL VENT LINE CHAFED AT WS 601.5 AND WS 656.5. (X)
- [SDR MZZA98159](https://openairdocs.org/sdr/MZZA98159.md): Switch · malfunctioned · May 22, 1998 · N69742 · Boeing 727224 · Leading Edge Slat Control System
  > FLT 956 - GUM - AFTER AIRBORNE, CREW CALLED TO ADVISED AIR RETURN DUE TO NR 1 LEADING EDGE FLAPS PROBLEM. NR 1 LE FLAPS DISAGREEMENT WITH FLAP HANDLE POSITION, RED INTRANSIT LIGHT STAYS ON. S/O PANEL SHOWS NR 1 LE FLAPS SHOWS DISAGREEMENT WITH FLAP HANDLE.
- [SDR MZZA97251](https://openairdocs.org/sdr/MZZA97251.md): Skin · corroded · Jul 17, 1997 · N69742 · Boeing 727224 · Fuselage Main, Plate/Skin
  > GUM - L/P 7948229. INTERGRANULAR CORROSION ON FS 1070 AND FS 1080 AT STR 29L. ALSO, STR 30, FORWARD OF STA 1070. CUT-OUT CORRODED AREAS ON FUSELAGE SKIN. FABRICATE AND INSTALL INTERIM REPAIR PER EC/RA 5330-02555 AND SRM 53-30-3, FIG 3. (X)
- [SDR MZZA9739](https://openairdocs.org/sdr/MZZA9739.md): Hyd Motor · failed · Mar 29, 1997 · N69742 · Boeing 727224 · Trailing Edge Flap Control System
  > FLT 918 - GUM - LOST A SYSTEM HYD DURING DESCENT INTO GUAM FROM SAIPAN. NO FLAP OR GEAR OR SPEED BRAKE EXTENDED. PERFORMED MANUAL EXTENSION OF GEAR AND FLAP USING PROCEDURES IN FLIGHT MANUAL. FOUND OUTBOARD FLAPS HYD DRIVE MOTOR LEAKING. REMOVED AND REPLAC
- [SDR MZZA97031](https://openairdocs.org/sdr/MZZA97031.md): Fuel Contl Unit · failed · Feb 19, 1997 · N69742 · Boeing 727224 · Fuel Control/Turbine Engines
  > GUM - FLT 915 - DURING CLIMB-OUT, NR 2 ENGINE WAS SHOWING ERRATIC INDICATION WHILE PASSING THROUGH 1000 FEET, EPR PLUS/MINUS.05, N1 PLUS 10 PERCENT, EGT PLUS/MINUS 50 DEGREES CELSIUS, N2 PLUS/MINUS 10 PERCENT, FUEL FLOW PLUS/MINUS 500 LBS. CREW AIR RETURN TO
- [SDR MZZA96140](https://openairdocs.org/sdr/MZZA96140.md): Wire · chafed · Nov 28, 1996 · N69742 · Boeing 727224 · Light System Wiring
  > GUM - DURING SERVICE CHECK, EMERGENCY AISLE PATH LIGHTS WOULD NOT TEST AT ROWS 17 TO 23, TROUBLESHOT AND FOUND FORWARD AND AFT BATTERY CHARGERS BLOWING FUSES. FOUND SHORTED WIRE AT SEAT 22B CHAFFING ON SEAT ASSEMBLY. REPAIRED WIRE AND REROUTED WIRE. REPLACE
- [SDR MZZA96116](https://openairdocs.org/sdr/MZZA96116.md): Frame · corroded · Oct 28, 1996 · N69742 · Boeing 727224 · Fuselage Main, Frame
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON FORWARD CARGO COMPARTMENT BS 480 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 28R AND STRINGER 27L. THE CORRODED FRAME LOWER CHORD FROM STRINGER 28L TO STRINGER 28R WAS TR
- [SDR MZZA96115](https://openairdocs.org/sdr/MZZA96115.md): Frame · corroded · Oct 28, 1996 · N69742 · Boeing 727224 · Fuselage Main, Frame
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 27R AND STRINGER 28R. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-4 FIGUR
- [SDR MZZA96114](https://openairdocs.org/sdr/MZZA96114.md): Frame · corroded · Oct 28, 1996 · N69742 · Boeing 727224 · Fuselage Main, Frame
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 28R AND STRINGER 29R. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-4 FIGUR
- [SDR MZZA96113](https://openairdocs.org/sdr/MZZA96113.md): Frame · corroded · Oct 28, 1996 · N69742 · Boeing 727224 · Fuselage Main, Frame
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 29R AND STRINGER 30. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-4 FIGURE
- [SDR MZZA96112](https://openairdocs.org/sdr/MZZA96112.md): Frame · corroded · Oct 28, 1996 · N69742 · Boeing 727224 · Fuselage Main, Frame
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 29L AND STRINGER 30. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-4 FIGURE
- [SDR MZZA96104](https://openairdocs.org/sdr/MZZA96104.md): Seat Track · corroded · Oct 27, 1996 · N69742 · Boeing 727224 · Fuselage, Seat/Cargo Attach Fittings
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK AT RBL 24.75 BETWEEN BS 1030 AND BS 1070. THE CORRODED SEAT TRACK FROM BS 1030 TO BS 1070 WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-5 F
- [SDR MZZA96118](https://openairdocs.org/sdr/MZZA96118.md): Frame · corroded · Oct 25, 1996 · N69742 · Boeing 727224 · Fuselage Main, Frame
  > TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1148 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 29L AND STRINGER 30. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-4 FIGURE
- [SDR MZZA96117](https://openairdocs.org/sdr/MZZA96117.md): Frame · corroded · Oct 25, 1996 · N69742 · Boeing 727224 · Fuselage Main, Frame
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARG COMPARTMENT BS 1148 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 29L AND STRINGER 28L. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-4 FIGURE
- [SDR MZZA96120](https://openairdocs.org/sdr/MZZA96120.md): Seat Track · corroded · Oct 24, 1996 · N69742 · Boeing 727224 · Fuselage, Seat/Cargo Attach Fittings
  > TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON PASSENGER CABIN SEAT TRACK FLANGE AT RBL 45.5 BETWEEN BS 1040 AND BS 1070. THE CORRODED SEAT TRACK FROM BS 1030 TO BS 1070 WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-1
- [SDR MZZA96125](https://openairdocs.org/sdr/MZZA96125.md): Stringer · corroded · Oct 23, 1996 · N69742 · Boeing 727224 · Fuselage Main, Longeron/Stringer
  > TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT AT THE FOLLOWING AREAS; BS 950 BULKHEAD LOWER CHORD BETWEEN STRINGER 29R AND STRINGER 28R, STRINGER 29R KEEL BEAM OUTBOARD FLANGE AT BS 950A. THE C
- [SDR MZZA96124](https://openairdocs.org/sdr/MZZA96124.md): Frame · corroded · Oct 23, 1996 · N69742 · Boeing 727224 · Fuselage Main, Frame
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 950F FRAME LOWER CHORD FLANGE BETWEEN STRINGER 29L AND STRINGER 28L. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-4 FIGUR
- [SDR MZZA96123](https://openairdocs.org/sdr/MZZA96123.md): Frame · corroded · Oct 23, 1996 · N69742 · Boeing 727224 · Fuselage Main, Frame
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 950F FRAME LOWER CHORD FLANGE BETWEEN STRINGER 27R AND STRINGER 28R. THE CORRODED FRAME LOWER CHORD WAS TRIMMED AND REPAIRED PER B727 SRM 53-10
- [SDR MZZA96122](https://openairdocs.org/sdr/MZZA96122.md): Frame · corroded · Oct 23, 1996 · N69742 · Boeing 727224 · Fuselage Main, Frame
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 970 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 27R AND STRINGER 28R. THE CORRODED FRAME LOWER CHORD WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53
- [SDR MZZA96121](https://openairdocs.org/sdr/MZZA96121.md): Frame · corroded · Oct 23, 1996 · N69742 · Boeing 727224 · Fuselage Main, Frame
  > TNN - DURING 1/4D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FUOND ON FORWARD CARGO COMPARTMENT BS 720C FRAME LOWER CHORD FLANGE BETWEEN STRINGER 25R AND STRINGER 26R. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B727 SRM 51-40-3 FI
- [SDR MZZA96111](https://openairdocs.org/sdr/MZZA96111.md): Frame · corroded · Oct 23, 1996 · N69742 · Boeing 727224 · Fuselage Main, Frame
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, SEVERE CORROSION WAS FOUND ON AFT CARGO COMPARTMENT BS 1130 FRAME LOWER CHORD FLANGE BETWEEN STRINGER 29L AND STRINGER 28L. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER B727 SRM 53-10-4 FIGUR
- [SDR MZZA96109](https://openairdocs.org/sdr/MZZA96109.md): Sign Cover · broken · Oct 21, 1996 · N69742 · Boeing 727224 · Emergency Lighting
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WAS FOUND ON FORWARD GALLEY AREA 'EXIT' SIGN COVER. THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-103 PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISF
- [SDR MZZA96108](https://openairdocs.org/sdr/MZZA96108.md): Sign Cover · broken · Oct 21, 1996 · N69742 · Boeing 727224 · Emergency Lighting
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WAS FOUND ON R1 GALLEY SERVICE DOOR 'EXIT' SIGN COVER. THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-106 PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SAT
- [SDR MZZA96107](https://openairdocs.org/sdr/MZZA96107.md): Sign Cover · broken · Oct 21, 1996 · N69742 · Boeing 727224 · Emergency Lighting
  > TNN - DURING 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, BROKEN COVER WAS FOUND ON L2 SERVICE DOOR 'EXIT' SIGN COVER. THE DAMAGED 'EXIT' SIGN ASSEMBLY WAS REMOVED AND REPLACED WITH P/N BR9279-105 PER B727 MM 33-50-11 AND OPERATIONAL CHECK FOUND SATISFACTO
- [SDR MZZA96106](https://openairdocs.org/sdr/MZZA96106.md): Batteries · discharged · Oct 21, 1996 · N69742 · Boeing 727224 · Emergency Lighting
  > TNN - DURNIG 1/4 D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, AFT AIRSTAIR CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. THE BATTERIES, P/N S106, WERE REMOVED AND REPLACED PER B727 MM 33-50-0 AND OPERATIONAL CHECK FOUND SATISFACTORY. REF, HANGAR NON RO
- [SDR MZZA96069](https://openairdocs.org/sdr/MZZA96069.md): Actuator · cracked · Aug 29, 1996 · N69742 · Boeing 727224 · Leading Edge Slat Actuator
  > FLT NR 916 - SPN - MAINTENANCE FOUND NR 3 LEADING EDGE SLAT LEAKING HYDRAULIC FLUID ON GROUND. MAINTENANCE REMOVED AND REPLACED NR 3 SLAT ACTUATOR DUE TO CRACK IN THE ACTUATOR HOUSING SYSTEM LEAK CHECK AND OPERATION CHECK GOOD, MM REFERENCE 27-81-22. (M)
- [SDR MZZA96066](https://openairdocs.org/sdr/MZZA96066.md): Connector · failed · Aug 18, 1996 · N69742 · Boeing 727224 · AC Power Distribution System
  > GUM - FLT 958 - SITTING AT GATE WITH APU RUNING, APU ELECTRICAL POWER KICKED OFF WITH A PHASE UNBALANCED LIGHT ON, ON ELECTRICAL FAULT PANEL. SHORTLY THEREAFTER, ELECTRICAL SMOKE IN COCKPIT. FOUND T3 TERMINAL ON 'A' PHASE FEEDER CABLE BURNED AT APU GENERATOR
- [SDR MZZA96057](https://openairdocs.org/sdr/MZZA96057.md): Skin · corrosion · Jul 9, 1996 · N69742 · Boeing 727224 · Fuselage Main, Plate/Skin
  > GUM - DURING B-CHECK, FOUND PREVIOUS SKIN REPAIR, LOWER BELLY, STATION 1030 TO STATION 1070, HAS IG CORROSION. REMOVED PREVIOUS SKIN REPAIR, REMOVED CORROSION PER SRM 51-10-6, ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED REPAIR DOUBLER FROM 2024 T3 SHEET
- [SDR MZZA95057](https://openairdocs.org/sdr/MZZA95057.md): Actuator · failed · Dec 31, 1995 · N69742 · Boeing 727224 · Leading Edge Slat Actuator
  > GUM - FLT NR 981 - AIRCRAFT DIVERTED BACK TO GUAM DUE TO LOSS OF 'A' SYSTEM HYDRAULIC QUANTITY. MAINTENANCE DISCOVERED THAT NR 5 LEADING EDGE SLAT ACTUATOR FAILED AND LEAKS. MECHANIC REMOVED AND REPLACED NR 5 LEADING EDGE SLAT ACTUATOR ASSY, SERVICED HYDRAUL
- [SDR MZZA95026](https://openairdocs.org/sdr/MZZA95026.md): Eel · inoperative · Apr 19, 1995 · N69742 · Boeing 727224 · Emergency Lighting
  > GUM - ON B-CHECK, MAINTENANCE FOUND R-1 SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. (W)
- [SDR CAL950307](https://openairdocs.org/sdr/CAL950307.md): Eel · inoperative · Apr 18, 1995 · N69742 · Boeing 727224 · Emergency Lighting
  > GUM - THE R-1 SERVICE DOOR EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE DURING B-CHECK. THE EMERGENCY EXIT LIGHT ASSEMBLY WAS REPLACED. (W)

## 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 = 'N69742' AND deregistration_id = 'N69742-2017-06-01'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N69742-2017-06-01/reports

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