# Service difficulty reports: N60312, cancelled Apr 3, 2006

A list on [N60312, cancelled Apr 3, 2006](https://openairdocs.org/deregistered/N60312-2006-04-03.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 · 68 reports

- [SDR CALA0500318](https://openairdocs.org/sdr/CALA0500318.md): Keelbeam · corroded · Sep 19, 2005 · N60312 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND LEFT KEELBEAM LOWER SURFACE CORRODED AT STA 663.75 TO 727. REPAIRED KEEL BEAM LOWER CHORD IAW ECRA 5311-01238.
- [SDR CALA0500317](https://openairdocs.org/sdr/CALA0500317.md): Keelbeam · corroded · Sep 19, 2005 · N60312 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND THE RIGHT KEEL BEAM CORRODED AT LOWER SURFACE BETWEEN STA 663.75 TO 696, S27R. REPAIRED IAW ECRA 5311-01239.
- [SDR CALA0400643](https://openairdocs.org/sdr/CALA0400643.md): Socket · shorted · Sep 19, 2004 · N60312 · Boeing 7373T0 · Passenger Compartment Lighting
  > SMOKE BEGAN COMING FROM THE FLOURESCENT SIDEWALL LIGHTING AT ROWS 18-19 ABC WHILE EN ROUTE FROM TUS TO IAH. THE HALON FIRE EXTINGUISHER WAS USED, LIGHTS WERE TURNED OFF, AND CIRCUIT BREAKERS WERE PULLED. THE SMOKE SUBSEQUENTLY CLEARED AND THE AIRCRAFT LANDED
- [SDR CALA0300460](https://openairdocs.org/sdr/CALA0300460.md): Fire Loop · damaged · Aug 8, 2003 · N60312 · Boeing 7373T0 · Fire Detection
  > THE APU FIRE LIGHT ILLUMINATED DURING CLIMBOUT OF DEN. THE FIRE HANDLE WAS PULLED AND THE FIRE BOTTLE WAS DISCHARGED. THE LIGHT WENT OUT, BUT ILLUMINATED AGAIN WITH THE FIRE BELL SOUNDED. THE AIRCRAFT WAS RETURNED TO DEN WHERE IT LANDED WITHOUT INCIDENT. M
- [SDR CALA0300387](https://openairdocs.org/sdr/CALA0300387.md): Frame · cracked · Jul 14, 2003 · N60312 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN RT MAIN FRAME ANGLE AT STA 616 FLOOR LINE. A STIFFENING ANGLE REPAIR WAS INSTALLED IAW ECRA 5311-01157.
- [SDR CALA0300382](https://openairdocs.org/sdr/CALA0300382.md): Support Angle · gouged · Jul 12, 2003 · N60312 · Boeing 7373T0 · Wing, Landing Gear Attach Fittings
  > INSPECTION FOUND LT MLG STAB LINK SUPPORT ANGLES GOUGED. THE ANGLES WERE REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0300370](https://openairdocs.org/sdr/CALA0300370.md): Frame · cracked · Jul 8, 2003 · N60312 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN LT MAIN FRAME ANGLE AT STA 616 BELOW FLOOR LINE, WL 200. REPAIRED FRAME IAW ECRA 5311-01154.
- [SDR CALA0300362](https://openairdocs.org/sdr/CALA0300362.md): Stringer · gouged · Jul 3, 2003 · N60312 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A GOUGE IN STRINGER AT STA 1120, RT, IN APU COMPARTMENT. THE DAMAGED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION OF STRINGER WAS INSTALLED IAW SRM 51-40-02.
- [SDR CALA0300361](https://openairdocs.org/sdr/CALA0300361.md): Floorbeam · corroded · Jul 3, 2003 · N60312 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED ON UPPER SURFACE AT STA 1006 BETWEEN RBL 24 AND RBL 32 AND RBL 27 INTERCOSTAL BS 1006-1016. A REPAIR WAS INSTALLED IAW SRM 53-00-51, FIGURE 202, PAGE 207-211.
- [SDR CALA0300357](https://openairdocs.org/sdr/CALA0300357.md): Seat Track · corroded · Jul 2, 2003 · N60312 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND THE LT I/B SEAT TRACK CORRODED BETWEEN BS 907 AND 947. A NEW SEAT TRACK SECTION WAS INSTALLED IAW SRM 53-00-52, FIGURE 204.
- [SDR CALA0300354](https://openairdocs.org/sdr/CALA0300354.md): Stringer · corroded · Jul 1, 2003 · N60312 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 27L CORRODED AT STA 1006. THE STRINGER WAS REPAIRED IAW SRM 53-00-03, FIGURE 201.
- [SDR CALA0300351](https://openairdocs.org/sdr/CALA0300351.md): Angle · corroded · Jul 1, 2003 · N60312 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-1 DOOR JAMB ZEE ANGLE CORRODED FROM BS 306-344. THE ZEE ANGLE WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0300350](https://openairdocs.org/sdr/CALA0300350.md): Angle · corroded · Jul 1, 2003 · N60312 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R-2 DOOR THRESHOLD Z-ANGLE CORRODED AT STA 937. THE ZEE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0300349](https://openairdocs.org/sdr/CALA0300349.md): Stringer · corroded · Jul 1, 2003 · N60312 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 26R CORRODED AT STA 1006-1016. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 5-40-2.
- [SDR CALA0300376](https://openairdocs.org/sdr/CALA0300376.md): Frame · cracked · Jun 30, 2003 · N60312 · Boeing 7373T0 · Fuselage Main, Frame
  > MAINTENANCE FOUND THE INNER CHORD ON THE LT FRAME AT STA 616 CRACKED. THE AREA WAS REPAIRED IAW ECRA 5311-01154.
- [SDR CALA0300347](https://openairdocs.org/sdr/CALA0300347.md): Channel · corroded · Jun 30, 2003 · N60312 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT AFT LAV FORWARD WALL LOWER U-CHANNEL CORRODED AT STA 986.5 - 1006. THE U-CHANNEL WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA0300345](https://openairdocs.org/sdr/CALA0300345.md): Web · cracked · Jun 30, 2003 · N60312 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND BOTTOM SURFACE OF R-2 DOOR THRESHOLD WEB CORRODED AT STA 986.5 TO 990. THE LOWER SILL WEB WAS REMOVED AND REPLACED IAW SRM 51-40-02.
- [SDR CALA0300343](https://openairdocs.org/sdr/CALA0300343.md): Galley Track · corroded · Jun 27, 2003 · N60312 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND GALLEY TRACK CORRODED BETWEEN BS 328 AND 360 AT RBL 44. THE FLOOR TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0300342](https://openairdocs.org/sdr/CALA0300342.md): Galley Track · corroded · Jun 27, 2003 · N60312 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CORROSION ON GALLEY TRACK BETWEEN BS 277 AND 294, RBL 44. THE GALLEY TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0101040](https://openairdocs.org/sdr/CALA0101040.md): Skin · cracked · Dec 23, 2001 · N60312 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 3/8" CRACK IN FUSELAGE SKIN AT STA 373, S28, E&E EXHAUST BAY CUTOUT. REPAIRED IAW ECRA 5330-02894.
- [SDR CALA0101035](https://openairdocs.org/sdr/CALA0101035.md): Web · gouged · Dec 21, 2001 · N60312 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A GOUGE IN WEB ON R/H SIDE OF E&E DOOR JAMB STRUCTURE AT STA 338, RBL 15. A DOUBLER WAS INSTALLED IAW SRM 51-70-13.
- [SDR CALA0101033](https://openairdocs.org/sdr/CALA0101033.md): Web · cracked · Dec 18, 2001 · N60312 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 1.25" AND 1" CRACK IN CENTER WEB OF FORWARD BULKHEAD AT STA 178, LBL 5.7, BETWEEN WL 195 AND 207. THE CENTER WEB WAS REPLACED IAW EA 5310-03040 AND WORK CARD 99-5310-1-0037.
- [SDR CALA0101032](https://openairdocs.org/sdr/CALA0101032.md): Keelbeam · corroded · Dec 18, 2001 · N60312 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND LT WHEEL KEEL BEAM O/B LOWER CHORD CORRODED AT STA 715-724. THE KEEL BEAM WAS REPAIRED IAW ECRA 5310-03740.
- [SDR CALA0101031](https://openairdocs.org/sdr/CALA0101031.md): Skin · gouged · Dec 17, 2001 · N60312 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN GOUGED BELOW FORWARD END OF DORSAL FIN ON R/H SIDE AT STA 876-885, RBL 5, S1-S2R. THE GOUGED AREA WAS REMOVED AND A DOUBLER WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.
- [SDR CALA0101030](https://openairdocs.org/sdr/CALA0101030.md): Torque Tube · corroded · Dec 14, 2001 · N60312 · Boeing 7373T0 · Service Doors
  > INSPECTION FOUND R-2 DOOR FUSELAGE TORQUE TUBE CORRODED. THE TORQUE TUBE WAS REMOVED AND REPLACED IAW MM 52-41-41.
- [SDR CALA9900818](https://openairdocs.org/sdr/CALA9900818.md): Stiffener · corroded · Jul 12, 1999 · N60312 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CORROSION ON CENTERLINE DOUBLE STIFFENER JUST AFT OF BS 1016 AT BOTTOM OF APB FORWARD SIDE. A NEW CHANNEL SECTION AND DOUBLERS WERE INSTALLED IAW SRM 53-80-08 AND 51-70-11.
- [SDR CALA9900817](https://openairdocs.org/sdr/CALA9900817.md): Floorbeam · corroded · Jul 12, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW ECRA 5310-03851.
- [SDR CALA9900816](https://openairdocs.org/sdr/CALA9900816.md): Skin · cracked · Jul 12, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.375 INCH CRACK IN THE RT LOWER KEEL BEAM SKIN PANEL BETWEEN STA 660 AND 670. A REPAIR WAS INSTALLED IAW ECRA 5330-02844.
- [SDR CALA9900814](https://openairdocs.org/sdr/CALA9900814.md): Gusset · cracked · Jul 8, 1999 · N60312 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN TORQUE BOX GUSSET AT STABILIZER CENTER SECTION, STA 1130. THE TORQUE BOX GUSSET WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA9900763](https://openairdocs.org/sdr/CALA9900763.md): Angle · corroded · Jun 30, 1999 · N60312 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND R-1 DOOR THRESHOLD FLOOR ATTACH ANGLE CORRODED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA9900760](https://openairdocs.org/sdr/CALA9900760.md): Skin · delaminated · Jun 30, 1999 · N60312 · Boeing 7373T0 · Ailerons
  > INSPECTION FOUND UPPER SURFACE OUTBOARD MID AREA OF LT AILERON DELAMINATED. THE AILERON WAS REPAIRED IAW ECRA 5761-01017.
- [SDR CALA9900813](https://openairdocs.org/sdr/CALA9900813.md): Track · corroded · Jun 29, 1999 · N60312 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND GALLEY TRACK CORRODED AT STA 290, RBL 45. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA9900751](https://openairdocs.org/sdr/CALA9900751.md): Angle · corroded · Jun 29, 1999 · N60312 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-2 PASSENGER DOOR THRESHOLD Z-ANGLE CORRODED FROM STA 914 TO 1006. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2.
- [SDR CALA9900750](https://openairdocs.org/sdr/CALA9900750.md): Floorbeam · corroded · Jun 29, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 328. THE UPPER SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA9900746](https://openairdocs.org/sdr/CALA9900746.md): Seat Track · corroded · Jun 28, 1999 · N60312 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LEFT O/B SEAT TRACK CORRODED AT STA 344 TO 362. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA9900745](https://openairdocs.org/sdr/CALA9900745.md): Floorbeam · corroded · Jun 28, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND LOWER SIDE OF FLOORBEAM CORRODED AT NUT PLATE, STA 294.5, LBL 48. THE CORRODED SECTION WAS REMOVED AND A NEW SECTION OF FLOORBEAM WAS INSTALLED IAW SRM 53-10-51, FIGURE 205.
- [SDR CALA9900743](https://openairdocs.org/sdr/CALA9900743.md): Floorbeam · corroded · Jun 28, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND TOP SIDE OF FLOORBEAM CORRODED AT STA 967, RBL 20 AND LBL 30. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR SECTION WAS INSTALLED IAW SRM 53-00-51.
- [SDR CALA9900742](https://openairdocs.org/sdr/CALA9900742.md): Floorbeam · corroded · Jun 28, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 312, LBL 17 TO RBL 38. INSTALLED REPAIR IAW SRM 53-00-51.
- [SDR CALA9900731](https://openairdocs.org/sdr/CALA9900731.md): Frame · cracked · Jun 27, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 4 INCH CRACK AT FASTENER HOLE OF FRAME AT STA 500, STRINGER 14R. THE CRACKED SECTION OF FRAME WAS CUT OUT. REPAIR DOUBLERS AND FILLER WERE INSTALLED IAW SRM 53-00-07, FIGURE 201.
- [SDR CALA9900729](https://openairdocs.org/sdr/CALA9900729.md): Support · cracked · Jun 26, 1999 · N60312 · Boeing 7373T0 · Nacelle/Pylon Structure
  > INSPECTION FOUND A 3 INCH CRACK IN NR 1 ENGINE DIAGONAL FRAME SUPPORT AT NACELLE STA 315 ON RT SIDE. THE DIAGONAL FRAME SUPPORT WAS REPLACED IAW SRM 51-40-02.
- [SDR CALA9900728](https://openairdocs.org/sdr/CALA9900728.md): Floorbeam · corroded · Jun 26, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 1006, LBL 30 TO RBL 11. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A REPAIR SECTION AND SPLICE WAS INSTALLED IAW SRM 53-00-51, FIGURE 202.
- [SDR CALA9900727](https://openairdocs.org/sdr/CALA9900727.md): Stringer · cracked · Jun 26, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A.5 INCH CRACK IN STRINGER 16L JUST AFT OF STA 500C. THE STRINGER WAS REPAIRED IAW SRM 53-00-03.
- [SDR CALA9900768](https://openairdocs.org/sdr/CALA9900768.md): Skin · cracked · Jun 25, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN FUSELAGE SKIN AT UPPER O/B CORNER OF L-1 WINDSHIELD. REPAIRED SKIN IAW ECRA 5330-02838.
- [SDR CALA9900721](https://openairdocs.org/sdr/CALA9900721.md): Frame · cracked · Jun 25, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK IN BELTFRAME AT STRINGER 16R AFT OF STA 500C. THE CRACKED SECTION OF FRAME WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-03, DETAIL VII.
- [SDR CALA9900719](https://openairdocs.org/sdr/CALA9900719.md): Floorbeam · corroded · Jun 24, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND CABIN FLOORBEAM CORRODED AT STA 294, RBL 35. THE CORROSION WAS REMOVED AND A NEW SECTION OF FLOORBEAM WAS SPLICED IN IAW SRM 53-10-51, FIGURE 205.
- [SDR CALA9900720](https://openairdocs.org/sdr/CALA9900720.md): Stringer · cracked · Jun 23, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 2 INCH CRACK IN STRINGER 4L AT STA 907. THE STRINGER WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA9900716](https://openairdocs.org/sdr/CALA9900716.md): Floorbeam · corroded · Jun 23, 1999 · N60312 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 1016. REPAIRED IAW ECRA 5310-03851.
- [SDR CALA9900631](https://openairdocs.org/sdr/CALA9900631.md): Torsion Link · broken · Jun 3, 1999 · N60312 · Boeing 7373T0 · Nose/Tail Landing Gear Strut/Axle
  > ON LANDING ROLL AT APPROXIMATELY 70 KNOTS WITH NORMAL NOSE WHEEL TOUCHDOWN, A VIOLENT SHIMMY WAS FELT ON RUNWAY UNTIL AIRCRAFT MADE A COMPLETE AND SAFE STOP. THERE WAS NO NOSE WHEEL STEERING CAPABILITY. THE AIRCRAFT WAS TOWED TO THE GATE. MAINTENANCE FOUND
- [SDR CALA9701251](https://openairdocs.org/sdr/CALA9701251.md): Circuit Card · inoperative · Aug 29, 1997 · N60312 · Boeing 7373T0 · Landing Gear Position and Warning
  > THE LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. THE GEAR LEVER WOULD NOT GO PAST THE OFF POSITION. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE COULD NOT DUPLICATE THE PROBLEM. THE PROBLEM WAS REPEATED ON A SUBSEQUENT FL
- [SDR CALA9701090](https://openairdocs.org/sdr/CALA9701090.md): Skin · cracked · Jul 8, 1997 · N60312 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 2 INCH CRACK IN LEFT ENGINE PYLON SKIN AT PANEL NR 5724. REPAIRED IAW ECRA 5430-01204.

Next page: https://openairdocs.org/deregistered/N60312-2006-04-03/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 = 'N60312' AND deregistration_id = 'N60312-2006-04-03'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N60312-2006-04-03/reports

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