# Service difficulty reports: N69333, cancelled Mar 21, 2013

A list on [N69333, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N69333-2013-03-21.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 · 55 reports

- [SDR CALA0800197](https://openairdocs.org/sdr/CALA0800197.md): Attach Fitting · cracked · Mar 5, 2008 · N69333 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > STA 384.2 LEFT SIDE S-15 ATTACH CLIP CRACKED. REMOVED AND REPLACED CRACKED CLIP AT BS 348.2 STRINGER 15 LT PER ECRA 5310-04726.
- [SDR CALA08](https://openairdocs.org/sdr/CALA08.md): Attach Fitting · cracked · Mar 5, 2008 · N69333 · Boeing 7373T0 · Fuselage Main, Attach Fittings
  > STA 384.2 LEFT SIDE S-15 ATTACH FITTING CRACKED. REMOVED AND REPLACED CRACKED ATTACH FITTING AT BS 348.2 STRINGER 15 LT PER ECRA 5310-04726.
- [SDR CALA0500422](https://openairdocs.org/sdr/CALA0500422.md): Spring · broken · Nov 29, 2005 · N69333 · Boeing 7373T0 · Escape Slide
  > THE R-2 DOOR AND L-2 DOOR ESCAPE SLIDE AFT GIRT BAR FLOOR BRACKETS WERE FOUND WITH SPRINGS BROKEN. NEW GIRT BAR FLOOR BRACKETS WERE INSTALLED AT BOTH AFT DOORS AT AFT POSITIONS IAW MM 25-61-51.
- [SDR CALA0500343](https://openairdocs.org/sdr/CALA0500343.md): Skin · cracked · Oct 9, 2005 · N69333 · Boeing 7373T0 · Cargo/Baggage Doors
  > AFT BAG BIN CARGO DOOR SKIN CRACKED AROUND HANDLE. INSTALLED DOUBLER PER SRM 52-00-01, 51-40-02, 51-20-05, 51-20-01.
- [SDR CALA0500342](https://openairdocs.org/sdr/CALA0500342.md): Frame · corroded · Oct 9, 2005 · N69333 · Boeing 7373T0 · Fuselage Main, Frame
  > AFT BAG BIN FLOOR FRAME STA 847 CORRODED AT SHEAR CLIPS. REPLACE FRAME SECTION PER SRM 51-10-02.
- [SDR CALA0500398](https://openairdocs.org/sdr/CALA0500398.md): Floorbeam · corroded · Oct 7, 2005 · N69333 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND THE RT SIDE OF UPPER CHORD OF FLOORBEAM CORRODED AT STA 1016, RBL 16 TO RBL 35. THE FLOORBEAM WAS REPAIRED BY SPLICING IN A NEW SECTION OF UPPER CHORD IAW ECRA 5321-01299.
- [SDR CALA0500340](https://openairdocs.org/sdr/CALA0500340.md): Bulkhead · corroded · Oct 7, 2005 · N69333 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > CORROSION AT STA 1016, BL 0, FWD LWR PRESSURE BULKHEAD. REPAIRED PER DRAWING 65C28106.
- [SDR CALA0500339](https://openairdocs.org/sdr/CALA0500339.md): Keelbeam · corroded · Oct 7, 2005 · N69333 · Boeing 7373T0 · Fuselage Main, Keel
  > LEFT KEELBEAM CORRODED FWD OF STA 500D. INSTALLED NEW SECTION OF KEEL BEAM PER SRM 53-60-12.
- [SDR CALA0500338](https://openairdocs.org/sdr/CALA0500338.md): Web · corroded · Oct 7, 2005 · N69333 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > AFT LEFT LAV PAN CORRODED. REPLACED LAV PAN PER SRM 51-40-01.
- [SDR CALA0500337](https://openairdocs.org/sdr/CALA0500337.md): Web · corroded · Oct 7, 2005 · N69333 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > AFT RIGHT LAV PAN CORRODED. REPLACED LAV PAN PER SRM 51-40-01.
- [SDR CALA0500329](https://openairdocs.org/sdr/CALA0500329.md): Skin · cracked · Oct 4, 2005 · N69333 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN BONDED DOUBLER LINE STA 767 BETWEEN S21R AND S22R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.
- [SDR CALA0500328](https://openairdocs.org/sdr/CALA0500328.md): Skin · cracked · Oct 4, 2005 · N69333 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN ON BONDED DOUBLER LINE STA 767 BETWEEN S22R AND S23R. A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.
- [SDR CALA050341](https://openairdocs.org/sdr/CALA050341.md): Bulkhead · damaged · Sep 30, 2005 · N69333 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > RIVET HOLE ELONGATED AT AFT PRESSURE BULKHEAD WEB, STA 1016, BL 0. INSTALLED SKIN PER DRAWING 65C28106.
- [SDR CALA0500322](https://openairdocs.org/sdr/CALA0500322.md): Floorbeam · corroded · Sep 29, 2005 · N69333 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND MAIN DECK FLOORBEAM CORRODED AT STA 344, LBL 16 TO RBL 9. THE SECTION OF FLOORBEAM WAS REPLACED IAW SRM 53-10-51.
- [SDR CALA0500323](https://openairdocs.org/sdr/CALA0500323.md): Floorbeam · corroded · Sep 28, 2005 · N69333 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND MAIN DECK FLOORBEAM CORRODED AT STA 328, RBL 42 TO LBL 35. THE FLOORBEAM SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.
- [SDR CALA0500376](https://openairdocs.org/sdr/CALA0500376.md): Wire Harness · burned · Sep 21, 2005 · N69333 · Boeing 7373T0 · Electrical Power System Wiring
  > FUEL SHUT-OFF VALVE WIRES & O/B LANDING LIGHT WIRES FOUND BURNED IN JUNCTION BOX NEAR D5164J (LANDING LIGHT DISCONNECT) AT RT SIDE AFT WHEEL WELL. SMOKE & COKING RESIDUE ON INSIDE SURFACE OF JUNCTION BOX COVER PLATE. ALL 3 LANDING LIGHT WIRES APPEARED TO HAV
- [SDR CALA0400234](https://openairdocs.org/sdr/CALA0400234.md): Skin · dented · Mar 10, 2004 · N69333 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A DENT IN AFT CARGO DOOR OUTER SKIN. THE DENTED AREA WAS CUT OUT. A REPAIR DOUBLER WAS INSTALLED IAW SRM 52-00-01, FIGURE 203.
- [SDR CALA0400181](https://openairdocs.org/sdr/CALA0400181.md): Strap · corroded · Feb 28, 2004 · N69333 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR STRAP CORRODED ALONG FASTENER HOLES AT BS 727D. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400178](https://openairdocs.org/sdr/CALA0400178.md): Angle · cracked · Feb 27, 2004 · N69333 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN MAIN CABIN FLOOR SHEAR WEB ANGLE AT STA 384, BL 0. THE SHEAR WEB ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400175](https://openairdocs.org/sdr/CALA0400175.md): Intercostal · cracked · Feb 26, 2004 · N69333 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN INTERCOSTAL AT STA 344, BL 0. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400163](https://openairdocs.org/sdr/CALA0400163.md): Flap · delaminated · Feb 25, 2004 · N69333 · Boeing 7373T0 · Trailing Edge Flaps
  > INSPECTION FOUND LEFT WING NR 1 AFT FLAP INBOARD T/E DELAMINATED. REPAIRED IAW SRM 51-70-10.
- [SDR CALA0300571](https://openairdocs.org/sdr/CALA0300571.md): Gearbox · failed · Oct 2, 2003 · N69333 · Boeing 7373T0 · Turbine Engine Accessory Drive
  > THE NR 2 ENGINE SUDDENLY AUTO SHUTDOWN WHILE CLIMBING THROUGH 19K AFTER TAKEOFF FROM EWR. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE TRANSFER GEARBOX AT FAULT. THE NR 2 ENGINE TRANSFER GEARBOX WAS REMOVED AND RE
- [SDR CALA0300024](https://openairdocs.org/sdr/CALA0300024.md): Pressure Panel · cracked · Jan 22, 2003 · N69333 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A CRACK IN THE PRESSURE DECK WEB AT STA 663, LBL 32. THE CRACK WAS ESTIMATED AT BEING.5 -.75 INCH LONG. A REPAIR WAS PERFORMED IAW SRM 53-60-51, FIGURE 203 AND ECRA 5310-04315.
- [SDR CALA0200451](https://openairdocs.org/sdr/CALA0200451.md): Pump · failed · Sep 6, 2002 · N69333 · Boeing 7373T0 · Engine Fuel Pump
  > THE NR 2 ENGINE FLAMED OUT WHILE ON DESCENT AT 10,000 FEET. AN ENGINE RESTART WAS ATTEMPTED, BUT WAS UNSUCCESSFUL. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FUEL PUMP AND MEC. LEAK AND OPERATIONAL CHECKS WERE GOOD. IN ADDI
- [SDR CALA0100989](https://openairdocs.org/sdr/CALA0100989.md): Skin · cracked · Oct 30, 2001 · N69333 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND CRACKS COMING FROM THREE RIVETS ON LOWER SIDE OF #6 SLAT SKIN BELOW I/B AUX TRACK. REPAIRED SLAT IAW SRM 57-43-01.
- [SDR CALA0100982](https://openairdocs.org/sdr/CALA0100982.md): Skin · cracked · Oct 28, 2001 · N69333 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND #1 SLAT SKIN CRACKED AT AFT ROW OF RIVETS APPROXIMATELY 1/8" ON EITHER SIDE OF RIVET, 43" O/B OF I/B END. A REPAIR WAS INSTALLED IAW SRM 57-43-01, FIGURE 206.
- [SDR CALA0100981](https://openairdocs.org/sdr/CALA0100981.md): Cargo Track · corroded · Oct 26, 2001 · N69333 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND TIE DOWN RAIL CORRODED AROUND FASTENER HOLES AT STA 727-945.5, RBL 26. THE CORRODED SECTIONS OF TIE DOWN RAIL WERE REMOVED AND REPLACED IAW SRM 53-00-53, FIGURE 202.
- [SDR CALA0100978](https://openairdocs.org/sdr/CALA0100978.md): Bracket · cracked · Oct 25, 2001 · N69333 · Boeing 7373T0 · Elevator Structure
  > LEFT ELEVATOR #4 HINGE UPPER ACCESS COVER OUTBOARD ATTACH BRACKET CRACKED. FABRICATED AND INSTALLED NEW BRACKET ON ELEVATOR PER SRM 51-40-01.
- [SDR CALA0100971](https://openairdocs.org/sdr/CALA0100971.md): Skin · dented · Oct 24, 2001 · N69333 · Boeing 7373T0 · Horizontal Stabilizer, Plate/Skin
  > DENT IN LEADING EDGE OF RIGHT HORIZONTAL STABILIZER AT STATION 263. PERFORMED INTERIM REPAIR PER SRM 55-10-01. PERMANENT REPAIR REQUIRED IN 18 MONTHS.
- [SDR CALA0100970](https://openairdocs.org/sdr/CALA0100970.md): Frame · dented · Oct 24, 2001 · N69333 · Boeing 7373T0 · Fuselage Main, Frame
  > FRAME 727B UPPER CAP DENTED AT S-21LT. FABRICATED AND INSTALLED REPAIR PER SRM 51-70-11.
- [SDR CALA0100969](https://openairdocs.org/sdr/CALA0100969.md): Keel · worn · Oct 24, 2001 · N69333 · Boeing 7373T0 · Fuselage Main, Keel
  > STRUCTURE AROUND HOLES FOR ATTACHMENT OF WHEEL WELL FAIRING WORN IN LEFT MLG. REPAIRED AREA ON KEEL REQUIRED BY EC/RA 5310-03740.
- [SDR CALA0100968](https://openairdocs.org/sdr/CALA0100968.md): Angle · worn · Oct 24, 2001 · N69333 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > T ANGLE ON FUSELAGE FORWARD END AT FILLET FAIRING SUPPORT ANGLE THAT ATTACHES TO UPPER WING TRAILING EDGE WORN. REMOVED AND REPLACED ANGLE PER SRM 51-10-2 AND 51-40-00.
- [SDR CALA0100966](https://openairdocs.org/sdr/CALA0100966.md): Floorbeam · corroded · Oct 22, 2001 · N69333 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > FLOORBEAM STATION 986.5 HAS SEVERAL CORRODED HOLES AT UPPER FLANGE (TOP AND BOTTOM). REPAIRED FLOORBEAM PER EC/RA 5310-03851.
- [SDR CALA0100965](https://openairdocs.org/sdr/CALA0100965.md): Skin · cracked · Oct 22, 2001 · N69333 · Boeing 7373T0 · Passenger/Crew Doors
  > L2 DOOR SKIN CRACKED AT UPPER HINGE CUT OUT (5/16"). REPAIRED PER SRM 52-00-01.
- [SDR CALA0100964](https://openairdocs.org/sdr/CALA0100964.md): Panel · corroded · Oct 22, 2001 · N69333 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > TRANSITION PANEL CORRODED AT BS 420 - 440 RIGHT. FABRICATED AND INSTALLED TRANSITION PANEL PER SRM 51-40-02.
- [SDR CALA0100963](https://openairdocs.org/sdr/CALA0100963.md): Seat Track · corroded · Oct 22, 2001 · N69333 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN RIGHT SIDE INBOARD SEAT TRACK CORRODED FROM STATION 727E TO STATION 767. REMOVED AND REPLACED SEAT TRACK PER SRM 53-00-52, SOPM 20-41-04 AND AMM 51-21-00.
- [SDR CALA0100962](https://openairdocs.org/sdr/CALA0100962.md): Web · cracked · Oct 18, 2001 · N69333 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > AFT LEFT AREA STATION 996 FLOOR WEB CRACKED (1 INCH) UNDER L2 Z-ANGLE. INSTALLED SERVICEABLE WEB WITH FASTENERS PER SRM 51-10-02.
- [SDR CALA0100960](https://openairdocs.org/sdr/CALA0100960.md): Seat Track · cracked · Oct 17, 2001 · N69333 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL 44 BS 328 - 380 CORRODED. CRACK (1/2") AT BS 380. REPAIRED PER SRM 53-00-02 AND 51-30-02.
- [SDR CALA0100956](https://openairdocs.org/sdr/CALA0100956.md): Angle · corroded · Oct 16, 2001 · N69333 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > CORROSION ON Z1 ANGLE AND ON L ANGLES BENEATH THE Z (BS 312-328 AND 328-344). REMOVED AND REPLACED ZEE ANGLES AND L-ANGLES PER SRM 51-10-02.
- [SDR CALA0100950](https://openairdocs.org/sdr/CALA0100950.md): Floor Support · cracked · Oct 15, 2001 · N69333 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT CRACKED AT SCREW HOLES BETWEEN STATIONS 927 AND 947.5 AT BL 0.0. FABRICATED AND INSTALLED SUPPORT ASSEMBLY PER SRM 51-10-2.
- [SDR CALA0100947](https://openairdocs.org/sdr/CALA0100947.md): Floorbeam · corroded · Oct 12, 2001 · N69333 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > FLOORBEAM BS 360, RBL 0-60, CORROSION UNDER G-2 GALLEY. REPAIRED FLOORBEAM IN REF TO SRM 53-00-51.
- [SDR CALA0100944](https://openairdocs.org/sdr/CALA0100944.md): Angle · cracked · Oct 12, 2001 · N69333 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > BS 294 BOX ANGLE CRACKED AT R1 DOOR CUT OUT JUST ABOVE FLOOR BEAM. TRIMMED CRACKED FLANGE. APPLIED ALODINE ADN PRIMER AND INSTALLED.050 FILLER PER EC/RA 5310-03895.
- [SDR CALA0100942](https://openairdocs.org/sdr/CALA0100942.md): Skin · cracked · Oct 11, 2001 · N69333 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1/2" CRACK IN L-1 WINDOW POST SKIN. THE CRACKED AREA OF SKIN WAS REMOVED AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 53-10-01.
- [SDR CALA9801336](https://openairdocs.org/sdr/CALA9801336.md): Circuit Breaker · popped · Jul 24, 1998 · N69333 · Boeing 7373T0 · Landing Gear Retraction/Extension System
  > THE GEAR HANDLE WOULD NOT MOVE PAST OFF POSITION AFTER TAKEOFF. THE AIRCRAFT WAS RETURNED TO ORD WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOOTING BY MAINTENANCE IAW MM 32-31-21, DUPLICATED CONTROL LEVER LOCK ON GROUND. THE LEVER LATCH CIRCUIT BREAKER WAS F
- [SDR CALA9800877](https://openairdocs.org/sdr/CALA9800877.md): Circuit Breaker · tripped · May 19, 1998 · N69333 · Boeing 7373T0 · Landing Gear Retraction/Extension System
  > THE GEAR LEVER WOULD NOT MOVE FROM THE OFF TO THE UP POSITION UPON GEAR RETRACTION AFTER TAKEOFF FROM IAH. CHECKLIST PROCEDURES WERE ACCOMPLISHED AND THE LOCK OVERRIDE TRIGGER WAS USED TO RETRACT THE GEAR. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WIT
- [SDR CALA9800724](https://openairdocs.org/sdr/CALA9800724.md): Wire · broken · Apr 29, 1998 · N69333 · Boeing 7373T0 · Light System Wiring
  > THE EMERGENCY TRACK LIGHTS AT LAST FIVE ROWS OF AIRCRAFT WERE FOUND INOPERATIVE DURING A PREFLIGHT CHECK. MAINTENANCE FOUND A WIRE BROKEN AT SEAT 21. THE WIRE WAS REPAIRED AND OPERATION OF THE LIGHTS WAS RESTORED.
- [SDR CALA971402](https://openairdocs.org/sdr/CALA971402.md): Chord · cracked · Oct 2, 1997 · N69333 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND A 3 CRACK IN LOWER T-CHORD AT NR 5 SLAT. THE T-CHORD WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA9701390](https://openairdocs.org/sdr/CALA9701390.md): Floorbeam · corroded · Sep 26, 1997 · N69333 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 294, RBL 10. THE FLOORBEAM WAS REPAIRED IAW SRM 53-10-51.
- [SDR CALA9700342](https://openairdocs.org/sdr/CALA9700342.md): Wire · shorted · Mar 13, 1997 · N69333 · Boeing 7373T0 · Light System Wiring
  > INSPECTION FOUND EMERGENCY EXIT FLOOR TRACK LIGHTING INOPERATIVE FROM ROWS 1 TO 7. A BLOWN FUSE WAS FOUND IN FORWARD BATTERY CHARGER. THE FUSE WAS REMOVED AND REPLACED. SHORTED WIRING WAS ALSO FOUND AT ROW 5. THE WIRING WAS REPAIRED AND OPERATION OF THE EME
- [SDR CALA9601135](https://openairdocs.org/sdr/CALA9601135.md): Fuel Control · inoperative · Aug 6, 1996 · N69333 · Boeing 7373T0 · Fuel Control/Turbine Engines
  > THE NR 1 ENGINE FLAMED OUT ON APPROACH TO IAH. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE FUEL CONTROL UNIT. THE FUEL PUMP WAS ALSO REPLACED. THE ENGINE WAS TRIMMED PER MM 71-00-01 AND ALL PARAMETERS WERE NORMAL

Next page: https://openairdocs.org/deregistered/N69333-2013-03-21/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 = 'N69333' AND deregistration_id = 'N69333-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N69333-2013-03-21/reports

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