# Service difficulty reports: N69348, cancelled Oct 8, 2009

A list on [N69348, cancelled Oct 8, 2009](https://openairdocs.org/deregistered/N69348-2009-10-08.md).

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

- [SDR CALA2009070100342](https://openairdocs.org/sdr/CALA2009070100342.md): Charger · intermittent · Jun 30, 2009 · N69348 · Boeing 7373T0 · Emergency Lighting
  > AFT EXIT DOOR EMERGENCY LIGHTS RIGHT AND LEFT SIDE ILUMINATED. REMOVED AND REPLACED BATTERY CHARGER, AND BATTERY PACK. OPS CHECKS GOOD.
- [SDR CALA2008122301163](https://openairdocs.org/sdr/CALA2008122301163.md): Skin · cracked · Dec 22, 2008 · N69348 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > STRINGER 24L, STATION 727E - 718 OUTER SKIN HAS 1 INCH CRACK. REPAIRED CRACK IN OUTER SKIN STRINGER 24L STATION 727 - 718 PER B737 SRM 53-00-01 FIG 201. TOTAL WEIGHT OF REPAIR, 9.84LBS FOR WEIGHT AND BALANCE CALCULATION.
- [SDR CALA2008122201162](https://openairdocs.org/sdr/CALA2008122201162.md): Intercostal · corroded · Dec 22, 2008 · N69348 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > FUSELAGE FRAME, SKIN AND SURROUNDING STRUCTURE CORRODED STATION 227.8 FROM LBL-12 TO RBL-12 (BILGE). REMOVED CORROSION FROM HORIZONTAL CHORD, FOUND TO BE WITHIN LIMITS, AND FOUND INTERCOSTAL TO BE OUT OF LIMITS. CLEANED AREA AND INSTALLED NEW INTERCOSTAL PER
- [SDR CALA2008122201159](https://openairdocs.org/sdr/CALA2008122201159.md): Skin · delaminated · Dec 20, 2008 · N69348 · Boeing 7373T0 · Leading Edge Devices
  > RIGHT WING NR 5 SLAT TRAILING EDGE WEDGE INBOARD AND OUTBOARD PROTECTIVE FINISH FOUND DELAMINATION ON OUTBOARD TRAILING EDGE. FABRICATED REPAIR DOUBLER AND REPLACED DAMAGED HONEYCOMB. BONDED REPAIR DOUBLER AND CORE, SEALED INBOARD AND OUTBOARD TRAILING EDGE
- [SDR CALA2008121901153](https://openairdocs.org/sdr/CALA2008121901153.md): Skin · delaminated · Dec 18, 2008 · N69348 · Boeing 7373T0 · Leading Edge Devices
  > LEFT WING NR 3 SLAT INBOARD END SKIN IS DELAMINATED. REPAIRED LEFT WING NR 3 SLAT TRAILING EDGE WEDGE PER SRM 51-70-10.
- [SDR CALA2008121901152](https://openairdocs.org/sdr/CALA2008121901152.md): Floorbeam · cracked · Dec 18, 2008 · N69348 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > FLOORBEAM BS 328 LBL 12 UPPER TEE CAP CRACKED SL-7 69. REPAIRED CRACKED FLOORBEAM AT BS 328 LBL 12 UPPER TEE CAP PER SRM 53-10-51 FIG 201.
- [SDR CALA2008121101138](https://openairdocs.org/sdr/CALA2008121101138.md): Door Frame · cracked · Dec 11, 2008 · N69348 · Boeing 7373T0 · Fuselage Main, Structure
  > FORWARD CARGO DOOR CUTOUT FORWARD FRAME CRACKED AT LOWER DOOR STOP FITTING AT STR 24R. REMOVED AND REPLACED FORWARD CARGO DOOR CUTOUT FORWARD FRAME PER SRM 51-10-2, PAGE 8, MAT ID 65-20722U70, PAC 59980.
- [SDR CALA0800700](https://openairdocs.org/sdr/CALA0800700.md): Skin · corroded · Jul 3, 2008 · N69348 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > GENERATED DIP DUE TO HEAVY CORROSION AT STATION 967, STR 27LT TO STR 27RT, PERFORM A PERMANET REPAIR PER EC/RA 5331-01244 WITHIN 6,000 FLIGHT CYCLES OR 24 MONTHS, WHICHEVER OCCURS FIRST. DURING OPEN-UP FOUND MORE CORROSION, REMOVED EXISTING REPAIRS AND REPAIR
- [SDR CALA0700525](https://openairdocs.org/sdr/CALA0700525.md): Actuator · inoperative · Sep 20, 2007 · N69348 · Boeing 737300 · Landing Gear Retraction/Extension System
  > THE LEFT MLG DID NOT INDICATE DOWN & LOCKED WHEN GEAR WAS EXTENDED ON APPROACH TO IAH. MANUAL EXTENSION WAS PERFORMED AND YAW WAS FELT WHEN LEFT MAIN EXTENDED. THE GEAR INDICATED 3 GREEN AND LANDING WAS NORMAL. THE GEAR WAS SWUNG SEVERAL TIMES WITH NO FAUL
- [SDR CALA0700490](https://openairdocs.org/sdr/CALA0700490.md): Controller · inoperative · Aug 20, 2007 · N69348 · Boeing 7373T0 · Cabin Pressure Controller
  > THE CREW RECEIVED A CABIN ALTITUDE WARNING CLIMBING THROUGH FL 270. THE QRH WAS FOLLOWED AND A RAPID DESCENT TO 13,000 FEET WAS ACCOMPLISHED. CABIN PRESSURE WAS RECOVERED VIA MANUAL DC. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT FURTHER PROBLE
- [SDR CALA0600239](https://openairdocs.org/sdr/CALA0600239.md): Brace · corroded · Jul 3, 2006 · N69348 · Boeing 7373T0 · Horizontal Stabilizer Structure
  > INSPECTION FOUND HORIZONTAL STABILIZER CENTER BRACE RT LOWER I/B CHORD CORRODED BETWEEN STA 1104 AND 1112. THE AREA WAS REPAIRED IAW ECRA 5510-01840.
- [SDR CALA0600238](https://openairdocs.org/sdr/CALA0600238.md): Frame · corroded · Jul 3, 2006 · N69348 · Boeing 7373T0 · Horizontal Stabilizer, Spar/Rib
  > INSPECTION FOUND HORIZONTAL STABILIZER CENTER BRACE LT LOWER I/B CHORD CORRODED BETWEEN STA 1121 AND 1129. THE AREA WAS REPAIRED IAW ECRA 5510-01841.
- [SDR CALA0600237](https://openairdocs.org/sdr/CALA0600237.md): Skin · corroded · Jul 3, 2006 · N69348 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND CORROSION ON AFT INTERIOR SURFACE OF THE LT WING AFT FUEL BOOST PUMP SKIN CUTOUT AT WS 70.85-140. A REPAIR WAS INSTALLED IAW ECRA 5720-01990.
- [SDR CALA0600236](https://openairdocs.org/sdr/CALA0600236.md): Skin · corroded · Jul 3, 2006 · N69348 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 967, S27R. A SKIN REPAIR WAS INSTALLED IAW ECRA 5331-01244.
- [SDR CALA0600228](https://openairdocs.org/sdr/CALA0600228.md): Floorbeam · cracked · Jul 1, 2006 · N69348 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND A 1.25 INCH CRACK ON THE TOP EDGE OF FLOORBEAM WEB AT STA 328, BL 0. A REPAIR WAS INSTALLED IAW ECRA 5321-01373.
- [SDR CALA0600227](https://openairdocs.org/sdr/CALA0600227.md): Stringer · cracked · Jun 30, 2006 · N69348 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1 INCH CRACK AT FORWARD PASSENGER DOOR CUTOUT ON STRINGER 15L SPLICE CHANNEL, STA 360, LBL 50. THE STRINGER WAS REPAIRED IAW ECRA 5311-01259 AND A DIP WAS ISSUED TO REINSPECT THE REPAIR WITHIN 6,000 FLIGHT CYCLES.
- [SDR CALA0600297](https://openairdocs.org/sdr/CALA0600297.md): Skin · cracked · Jun 29, 2006 · N69348 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A CRACK AT THREE EACH LIGHTENING HOLES ON THE INNER SKIN OF THE FORWARD CARGO DOOR. THE SKIN WAS REPAIRED IAW ECRA 5232-01076.
- [SDR CALA0600223](https://openairdocs.org/sdr/CALA0600223.md): Skin · cracked · Jun 28, 2006 · N69348 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 765 JUST ABOVE STRINGER 21R ON BONDED DOUBLER LINE. THE CRACKED SECTION OF SKIN WAS CUT OUT AND A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-00-0, REPAIR 31, PROCEDURE V, DETAIL VII, FIGURE 201, PAGE 228.
- [SDR CALA0600221](https://openairdocs.org/sdr/CALA0600221.md): Floorbeam · corroded · Jun 26, 2006 · N69348 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND MAIN CABIN FLOORBEAM CORRODED AT STA 328, RBL 11-36. REPLACED T-CAP ON FLOORBEAM IAW SRM 53-10-5, REPAIR 5.
- [SDR CALA0600218](https://openairdocs.org/sdr/CALA0600218.md): Beltframe · corroded · Jun 24, 2006 · N69348 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FORWARD BAGGAGE BIN BELT FRAME CORRODED AT STA 500D, S27L, LBL11-13. A DOUBLER WAS INSTALLED IAW SRM 53-00-07 FIGURE 201 REPAIR 7.
- [SDR CALA0600217](https://openairdocs.org/sdr/CALA0600217.md): Beltframe · corroded · Jun 23, 2006 · N69348 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND FORWARD BAGGAGE BIN BELT FRAME CORRODED AT STA 480, S27L, LBL 13-17. REPAIRED IAW SRM 53-00-07.
- [SDR CALA0600214](https://openairdocs.org/sdr/CALA0600214.md): Angle · corroded · Jun 21, 2006 · N69348 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-2 DOOR Z-ANGLE CORRODED AT STA 947-999, LBL 40. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0600224](https://openairdocs.org/sdr/CALA0600224.md): Frame · cracked · May 13, 2006 · N69348 · Boeing 7373T0 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1.5 INCH CRACK IN THE FORWARD CARGO DOOR LOWER CORNER FRAME JUST BELOW DOOR HOLD OPEN HOOK. THE DOOR FRAME WAS REPAIRED IAW SRM 51-40-02 AND EA 5230-01030.
- [SDR CALA0500324](https://openairdocs.org/sdr/CALA0500324.md): Wire · shorted · Oct 3, 2005 · N69348 · Boeing 7373T0 · Light System Wiring
  > THE FIRST CLASS EMERGENCY ESCAPE AISLE PATH LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE FOUND SHORTED WIRING TO TRANSFORMER. THE WIRING WAS REPAIRED AND OPERATIONAL CHECKS WERE GOOD.
- [SDR CALA0400713](https://openairdocs.org/sdr/CALA0400713.md): Skin · cracked · Nov 9, 2004 · N69348 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 2 INCH CRACK IN FUSELAGE SKIN BELOW FASTENER ROW BETWEEN STA 727E AND 747, S24R. A REPAIR DOUBLER AND TRIPLER WERE INSTALLED IAW SRM 53-00-01, FIGURE 229.
- [SDR CALA0400584](https://openairdocs.org/sdr/CALA0400584.md): Skin · corroded · Jul 23, 2004 · N69348 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED AND CRACKED AT STA 259.5-360, S24L TO S29L. THE SKIN WAS REMOVED AND REPLACED IAW ECRA 5310-04421.
- [SDR CALA0400535](https://openairdocs.org/sdr/CALA0400535.md): Skin · cracked · Jun 13, 2004 · N69348 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1.5 INCH CRACK IN FUSELAGE SKIN AT STA 747, STRINGER 23L. DOUBLERS WERE INSTALLED IAW SRM 53-00-01, FIGURE 229.
- [SDR CALA0300044](https://openairdocs.org/sdr/CALA0300044.md): Skin · cracked · Feb 12, 2003 · N69348 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 3" CRACK IN FUSELAGE SKIN AT STA 727A, S23L. REPAIRED IAW ECRA 5330-03090.
- [SDR CALA0200352](https://openairdocs.org/sdr/CALA0200352.md): Keelbeam · corroded · Jun 19, 2002 · N69348 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND KEEL BEAM LT LOWER O/B CHORD CORRODED AT STA 727. REPAIRED IAW ECRA 5311-01127.
- [SDR CALA0200351](https://openairdocs.org/sdr/CALA0200351.md): Skin · cracked · Jun 18, 2002 · N69348 · Boeing 7373T0 · Leading Edge Devices
  > INSPECTION FOUND #6 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01.
- [SDR CALA0200339](https://openairdocs.org/sdr/CALA0200339.md): Seat Track · corroded · Jun 13, 2002 · N69348 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND MAIN CABIN FLOOR R/H I/B SEAT TRACK HAD CORROSION AND WORN LOBES AT BS 787 AND 797, THE CORRODED AND WORN SECTION OF SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK SECTION WAS SPLICED IN IAW SRM 53-00-52, FIGURE 204.
- [SDR CALA0200337](https://openairdocs.org/sdr/CALA0200337.md): Seat Track · corroded · Jun 12, 2002 · N69348 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND L/H I/B SEAT TRACK CORRODED AT STA 907-940. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.
- [SDR CALA0200335](https://openairdocs.org/sdr/CALA0200335.md): Seat Track · corroded · Jun 10, 2002 · N69348 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND R/H I/B SEAT TRACK CORRODED AT STA 907-935. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-60-52.
- [SDR CALA0200332](https://openairdocs.org/sdr/CALA0200332.md): Strap · corroded · Jun 8, 2002 · N69348 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R/H SIDE Y STRAP CORRODED FROM STA 1006 TO AFT PRESSURE BULKHEAD, RBL 6. THE STRAP WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0200331](https://openairdocs.org/sdr/CALA0200331.md): Floor Support · corroded · Jun 7, 2002 · N69348 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT UNDER R2 DOOR Z-ANGLE AT STA 969 CORRODED. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02, 51-40-02, AND 51-30-01.
- [SDR CALA0200330](https://openairdocs.org/sdr/CALA0200330.md): Seat Track · corroded · Jun 7, 2002 · N69348 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACK CORRODED AT STA 270-294, RBL 43. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0000552](https://openairdocs.org/sdr/CALA0000552.md): Harness · broken · Apr 25, 2000 · N69348 · Boeing 7373T0 · Emergency Lighting
  > EMERGENCY AISLE PATH LIGHTING INOP AT ROW 6 AND 22. REPLACED WIRE HARNESS AT BOTH ROWS PER MAINTENANCE MANUAL 33-51-02 PG 501.
- [SDR CALA9900540](https://openairdocs.org/sdr/CALA9900540.md): Trigger · out of position · May 10, 1999 · N69348 · Boeing 7373T0 · Passenger/Crew Doors
  > FORWARD ENTRY DOOR WILL NOT OPEN. FOUND RELEASE LATCH MECHANISM DISSASSEMBLED AND TRIGGER OUT OF POSITION. REASSEMBLED AND TESTED PER MM 52-11-00 PAGE 501.
- [SDR CALA9801501](https://openairdocs.org/sdr/CALA9801501.md): Stringer · corroded · Aug 24, 1998 · N69348 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER CORRODED JUST BELOW RT AFT LAV DUMP CHUTE FROM STA 1006 TO 1016. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION OF STRINGER AND SHIM WERE FABRICATED AND INSTALLED IAW ECRA 5360-01018.
- [SDR CALA9801487](https://openairdocs.org/sdr/CALA9801487.md): Floorbeam · corroded · Aug 20, 1998 · N69348 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FORWARD GALLEY FLOORBEAM CORRODED AT STA 344, LBL 30 TO 20. THE FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA9801486](https://openairdocs.org/sdr/CALA9801486.md): Floorbeam · corroded · Aug 19, 1998 · N69348 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 312, RBL 15 AND LBL 20. REPAIR DOUBLERS WERE INSTALLED IAW SRM 53-10-51.
- [SDR CALA9800721](https://openairdocs.org/sdr/CALA9800721.md): Oven · dirty · Apr 29, 1998 · N69348 · Boeing 7373T0 · Buffet/Galleys
  > THE CREW REPORTED SMOKE COMING FROM NR 1 AND NR 2 AFT GALLEY OVENS IN FLIGHT. THE SMOKE WAS MOMENTARY. THE FLIGHT WAS CONTINUED TO DEN WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND NO EVIDENCE OF FIRE. FOOD RESIDUE WAS FOUND ON THE HEATING ELEMENTS OF BOTH OV
- [SDR CALA9800016](https://openairdocs.org/sdr/CALA9800016.md): Logic Card · inoperative · Jan 12, 1998 · N69348 · Boeing 7373T0 · Landing Gear Position and Warning
  > THE RT MLG INDICATION WAS SHOWING RED AND GREEN AFTER GEAR RETRACTION. THE GEAR WAS CYCLED AND THE RED LIGHT EXTINGUISHED. THE RED LIGHT ILLUMINATED INTERMITTENTLY DURING FLIGHT. MAINTENANCE FOUND THE M986 LOGIC CARD AT FAULT. THE M986 LOGIC CARD WAS REMOV
- [SDR CALA9701711](https://openairdocs.org/sdr/CALA9701711.md): Tire · failed · Dec 6, 1997 · N69348 · Boeing 7373T0 · Tire
  > A LT MLG TIRE BLEW ON TAKEOFF, THE A-HYD SYSTEM PRESSURE AND QUANTITY WAS LOST. THE AIRCRAFT WAS RETURNED. UPON LANDING THE OTHER LT MLG TIRE BLEW. THE BLOWN TIRES HAD DAMAGED THE LEFT INBOARD AFT FLAP, THE LT INBOARD MLG DOOR, THE LEFT GEAR DOWNLOCK AFT SP
- [SDR CALA9700971](https://openairdocs.org/sdr/CALA9700971.md): Windshield · failed · Jun 26, 1997 · N69348 · Boeing 7373T0 · Flight Compartment Windows
  > A STRONG ODOR ACCOMPANIED BY SMOKE WAS OBSERVED IN THE COCKPIT DURING CLIMB-OUT OF DTW ENROUTE TO EWR. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FIRST OFFICER'S NR 5 WINDOW OVERHEATING AND CAUSING THE ODOR AND SMO
- [SDR CALA9601302](https://openairdocs.org/sdr/CALA9601302.md): Angle · cracked · Sep 4, 1996 · N69348 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1 INCH CRACK IN ANGLE AT STA 540, STRINGER 22R. THE CRACKED AREA WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 51-70-11.
- [SDR CAL960191](https://openairdocs.org/sdr/CAL960191.md): Rollers/Tracks · lack of lube · Feb 25, 1996 · N69348 · Boeing 7373T0 · Leading Edge Devices
  > FLT NR 1708 - EWR - WHEN FLAPS WERE SELECTED BEYOND 5 DEGREES CREW RECEIVED T/E FLAP ASYMMETRY. THE SAFETY WIRES WERE BROKEN ON GPWS AND ALTERNATE FLAP MASTER SWITCH. THE LEFT INDICATOR WENT TO 10 DEGREES AND THE RIGHT STAYED AT 5 DEGREES. THE AIRCRAFT WAS

## 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 = 'N69348' AND deregistration_id = 'N69348-2009-10-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N69348-2009-10-08/reports

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