# Service difficulty reports: N70353, cancelled Aug 23, 2012

A list on [N70353, cancelled Aug 23, 2012](https://openairdocs.org/deregistered/N70353-2012-08-23.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 · 66 reports

- [SDR CALA0600374](https://openairdocs.org/sdr/CALA0600374.md): Door Frame · cracked · Oct 2, 2006 · N70353 · Boeing 7373T0 · Fuselage Main, Structure
  > INSPECTION FOUND A.5 INCH CRACK IN FWD BAG BIN DOOR CUTOUT AFT FRAME NR 5 STOP PAD, STA 480-500, S16R - S27R. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.
- [SDR CALA0500239](https://openairdocs.org/sdr/CALA0500239.md): Skin · cracked · Jul 30, 2005 · N70353 · Boeing 7373TO · Fuselage Main, Plate/Skin
  > A 2 INCH CRACK WAS FOUND IN FUSELAGE SKIN BELOW THE LT REAR EXTERIOR EMERGENCY EXIT LIGHT, STA 727D - 727E, S23L DURING WALKAROUND. DOUBLERS WERE INSTALLED IAW ECRA 5330-03469. A DIP WAS ISSUED TO PERFORM AN INITIAL INSPECTION WITHIN 60,000 FLIGHT CYCLES FRO
- [SDR CALA0400440](https://openairdocs.org/sdr/CALA0400440.md): Brace · cracked · May 1, 2004 · N70353 · Boeing 7373T0 · Nacelle/Pylon Miscellaneous Structure
  > INSPECTION FOUND A 3 INCH CRACK IN NR 1 ENGINE AFT LOWER PYLON AREA DIAGONAL BRACE. THE DIAGONAL BRACE WAS REMOVED AND REPLACED IAW MM 54-10-01.
- [SDR CALA0400495](https://openairdocs.org/sdr/CALA0400495.md): Floorbeam · cracked · Apr 28, 2004 · N70353 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > A CRACK WAS FOUND IN THE LONGITUDINAL FLOORBEAM UPPER CHORD AT ITS ATTACHMENT TO THE TRANSVERSE FLOORBEAM AT STA 727B, RBL 45. THE CRACK WAS LOCATED ON THE I/B SIDE OF THE LONGITUDINAL FLOORBEAM AT THE SECOND HI-LOK FASTENER HOLE FORWARD OF STA 727B. THE CRA
- [SDR CALA0400435](https://openairdocs.org/sdr/CALA0400435.md): Bearing · damaged · Apr 28, 2004 · N70353 · Boeing 7373T0 · Nose/Tail Landing Gear Attach Section
  > NOSE GEAR, LEFT TRUNNION BEARING IN BULKHEAD PITTED. REPAIRED PER ECRA 53543-01013.
- [SDR CALA0400434](https://openairdocs.org/sdr/CALA0400434.md): Bearing · damaged · Apr 27, 2004 · N70353 · Boeing 7373T0 · Nose/Tail Landing Gear Attach Section
  > NOSE GEAR, RIGHT TRUNNION BEARING IN BULKHEAD FITTING PITTED. REPAIRED PER ECRA 5343-01013.
- [SDR CALA0400432](https://openairdocs.org/sdr/CALA0400432.md): Fitting · corroded · Apr 27, 2004 · N70353 · Boeing 7373T0 · Fuselage, Stabilizer Attach Fittings
  > VERTICAL STABILIZER AFT LEFT ATTACH LUG, AFT FAILSAFE FITTING CORRODED. INSTALLED NEW FITTING PER SRM 51-40-02 & 51-40-03.
- [SDR CALA0400431](https://openairdocs.org/sdr/CALA0400431.md): Fitting · corroded · Apr 27, 2004 · N70353 · Boeing 7373T0 · Fuselage, Stabilizer Attach Fittings
  > VERTICAL STABILIZER AFT ATTACH LUG, FWD FAILSAFE FITTING CORRODED. INSTALLED NEW FITTING PER SRM 51-40-02 & 51-40-03.
- [SDR CALA0400430](https://openairdocs.org/sdr/CALA0400430.md): Intercostal · worn · Apr 27, 2004 · N70353 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CHANNEL BELOW APU BLEED AIR DUCT AT STA 639 WORN. REPLACED INTERCOSTAL PER SRM 51-10-2.
- [SDR CALA0400429](https://openairdocs.org/sdr/CALA0400429.md): Stick Shaker · will not test · Apr 27, 2004 · N70353 · Boeing 7373T0 · Stall Warning System
  > CAPTAINS STICK SHAKER WILL NOT TEST. REPLACED STICK SHAKER PER AMM 27-32-31.
- [SDR CALA0400422](https://openairdocs.org/sdr/CALA0400422.md): Skin · dented · Apr 25, 2004 · N70353 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > FUSELAGE DENT AFT OF BS 986.5+4, 12 INCHES ABOVE DRAIN MAST. REPAIRED PER SRM 53-00-01.
- [SDR CALA0400421](https://openairdocs.org/sdr/CALA0400421.md): Skin · dented · Apr 25, 2004 · N70353 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > FUSELAGE DENTED AT BS 1006 MINUS 4 INCHES, 12 INCHES ABOVE DRAIN MAST. REPAIRED PER SRM 53-00-01.
- [SDR CALA0400420](https://openairdocs.org/sdr/CALA0400420.md): Skin · dented · Apr 25, 2004 · N70353 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED BETWEEN STA 986.5 AND 1006, 3 PLACES,.1562 INCH DIA. REPAIRED PER SRM 53-00-01.
- [SDR CALA0400418](https://openairdocs.org/sdr/CALA0400418.md): Frame · cracked · Apr 24, 2004 · N70353 · Boeing 7373T0 · Fuselage Main, Frame
  > UPPER FLANGE CRACKED AT STA 500 1 X 1 INCH. INSTALLED DOUBLER PER SRM 51-70-11, FIG 1.
- [SDR CALA0400417](https://openairdocs.org/sdr/CALA0400417.md): Seat Track · worn · Apr 24, 2004 · N70353 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > CAPTAINS SEAT TRACK WORN, 6 HOLES. REPLACED TRACK PER AMM 25-11-11.
- [SDR CALA0400416](https://openairdocs.org/sdr/CALA0400416.md): Seat Track · worn · Apr 24, 2004 · N70353 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > FIRST OFFICERS SEAT TRACK WORN, 6 HOLES. REPLACED SEAT TRACK PER 25-11-11.
- [SDR CALA0400409](https://openairdocs.org/sdr/CALA0400409.md): Mount Bracket · cracked · Apr 23, 2004 · N70353 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > CRACK (3.5 INCH) IN MOUNT FOR NUMBER TWO VHF ANTENNA IN FORWARD CARGO COMPARTMENT. REPLACED MOUNT PER SRM 51-40-02.
- [SDR CALA0400386](https://openairdocs.org/sdr/CALA0400386.md): Stringer · corroded · Apr 18, 2004 · N70353 · Boeing 7373T0 · Fuselage Main, Longeron/Stringer
  > STRINGER 27L HAS HEAVY CORROSION FROM STA 955 TO APB (5 FT). REMOVED AND REINSTALLED NEW STRINGER SECTION AT 27 LEFT STA 907 TO 1016 PER SRM 51-10-02.
- [SDR CALA0400390](https://openairdocs.org/sdr/CALA0400390.md): Seat Track · corroded · Apr 16, 2004 · N70353 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK CORRODED (10 INCHES) BETWEEN FLOOR STATION 328 AND 346. REPLACED CORRODED SEAT TRACK PER SRM 53-00-52.
- [SDR CALA0400389](https://openairdocs.org/sdr/CALA0400389.md): Mount · corroded · Apr 16, 2004 · N70353 · Boeing 7373T0 · Fuselage, Equipment Attach Fittings
  > FORWARD LAV MOUNT CORRODED AT STA 300 LBL 10. REMOVED AND REPLACED DAMAGED MOUNT PER SRM 51-10-02.
- [SDR CALA0400388](https://openairdocs.org/sdr/CALA0400388.md): Mount · corroded · Apr 16, 2004 · N70353 · Boeing 7373T0 · Fuselage, Equipment Attach Fittings
  > FORWARD CABIN LAV MOUNT AT STATION 300 LBL 42 CORRODED. REMOVED AND REPLACED MOUNT PER SRM 51-10-02.
- [SDR CALA0400387](https://openairdocs.org/sdr/CALA0400387.md): Floorbeam · corroded · Apr 16, 2004 · N70353 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > PAX FLOOR STATION 312 FLOORBEAM STRAP HAS LITE CORROSION. INSTALLED NEW SECTION OF FLOORBEAM PER SRM 53-10-51.
- [SDR CALA0400374](https://openairdocs.org/sdr/CALA0400374.md): Shear Web · cracked · Apr 15, 2004 · N70353 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN AFT CABIN SHEAR WEB AT STA 927-947.5, BL 0. A REPAIR WAS INSTALLED IAW BOEING DRAWING 69-36656.
- [SDR CALA0400371](https://openairdocs.org/sdr/CALA0400371.md): Channel · corroded · Apr 14, 2004 · N70353 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND L-1 DOOR CUTOUT CHANNEL CORRODED AT STA 312-344. THE CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400370](https://openairdocs.org/sdr/CALA0400370.md): Bracket · corroded · Apr 14, 2004 · N70353 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR BRACKET (GIRT BAR TIE DOWN) CORRODED AT STA 312, LBL 52. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400369](https://openairdocs.org/sdr/CALA0400369.md): Bracket · corroded · Apr 14, 2004 · N70353 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR BRACKET (GIRT BAR LATCH TIE DOWN) AT STA 344, LBL 54 CORRODED. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-02.
- [SDR CALA0400367](https://openairdocs.org/sdr/CALA0400367.md): Seat Track · corroded · Apr 14, 2004 · N70353 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACK CORRODED AT STA 270-294, RBL 40. THE SEAT TRACK WAS REPLACED IAW SRM 51-10-02.
- [SDR CALA0400361](https://openairdocs.org/sdr/CALA0400361.md): Bulkhead · wrinkled · Apr 13, 2004 · N70353 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND STRAP ON AFT FACE OF AFT PRESSURE BULKHEAD BULDGED/WRINKLED BETWEEN STRINGER 6L AND 8L, LBL 40. THE STRAP WAS REMOVED AND A REPAIR STRAP AND FILLER WERE INSTALLED IAW ECRA 5310-04310.
- [SDR CALA0400048](https://openairdocs.org/sdr/CALA0400048.md): Panel · cracked · Jan 21, 2004 · N70353 · Boeing 7373T0 · Wing, Plate/Skin
  > INSPECTION FOUND A.75 INCH CRACK IN RT WING NR 6 SLAT AUX TRACK AT I/B AUX TRACK CUTOUT (FIXED L/E PANEL). THE CRACK WAS STOP DRILLED IAW SRM 57-41-01, FIGURE 101, SHEET 4, NOTE O AND P. THE CRACK WAS PLACED ON DIP TO REINSPECT EVERY 400 HOURS AND REPAIR WI
- [SDR CALA0200580](https://openairdocs.org/sdr/CALA0200580.md): Web · corroded · Dec 10, 2002 · N70353 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND UPPER SURFACE OF AFT BAGGAGE BIN LOWER THRESHOLD WEB CORRODED. THE THRESHOLD WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.
- [SDR CALA0200578](https://openairdocs.org/sdr/CALA0200578.md): Skin · cracked · Dec 9, 2002 · N70353 · Boeing 7373T0 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 0.15" CRACK IN SKIN AT A/C ACCESSORY COOLING EXHAUST OUTLET ON AFT SIDE, STA 380, S27L. A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5330-02894.
- [SDR CALA0200574](https://openairdocs.org/sdr/CALA0200574.md): Floorbeam · corroded · Dec 6, 2002 · N70353 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT FASTENER HOLE, STA 312, RBL 37. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND REPLACED IAW SRM 53-10-51.
- [SDR CALA0200573](https://openairdocs.org/sdr/CALA0200573.md): Keelbeam · worn · Dec 5, 2002 · N70353 · Boeing 7373T0 · Fuselage Main, Keel
  > INSPECTION FOUND THREE FASTENER HOLES WITH WASHERS THAT HAD WORN INTO THE KEEL BEAM ON LT SIDE I/B OF MLG WHEEL WELL AT STA 699-727. A REPAIR WAS INSTALLED IAW ECRA 5310-03740, REV A.
- [SDR CALA0200563](https://openairdocs.org/sdr/CALA0200563.md): Diode · disconnected · Nov 24, 2002 · N70353 · Boeing 7373T0 · Landing Gear Selector
  > THE LANDING GEAR WOULD NOT RAISE AFTER TAKEOFF FROM RDU. THE GEAR HANDLE WOULD NOT MOVE PAST THE OFF POSITION. THE AIRCRAFT WAS RETURNED TO RDU WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT JUMPER, DIODE M416, ON BACK OF THE GEAR LEVER ASSEMBLY WAS
- [SDR CALA0200155](https://openairdocs.org/sdr/CALA0200155.md): Diode · faulty · Mar 28, 2002 · N70353 · Boeing 7373T0 · Landing Gear Retraction/Extension System
  > THE LANDING GEAR TRIGGER LOCK OVERRIDE WAS REQUIRED TO RAISE THE GEAR AFTER TAKEOFF FROM EWR. IN ADDITION, THE "LAND GEAR LATCH AND PRESS WARNING" CIRCUIT BREAKER POPPED AND WOULD NOT RESET. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED SAFELY. MAINTENANCE
- [SDR CALA0001332](https://openairdocs.org/sdr/CALA0001332.md): Bulkhead · cracked · Aug 26, 2000 · N70353 · Boeing 7373T0 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A.25 INCH CRACK ON FORWARD BULKHEAD AT STA 178, RBL 5.7, WL 198. THE AREA WAS REPAIRED IAW EA 5310-03040 AND ECRA 5310-04037.
- [SDR CALA0001230](https://openairdocs.org/sdr/CALA0001230.md): Floorbeam · mismanufactured · Aug 7, 2000 · N70353 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > THE RT SIDE FLOORBEAM AT BS 1016 WAS FOUND TO HAVE AN INSUFFICIENT NUMBER OF FASTENERS DURING ACCOMPLISHMENT OF FCD 5321-01052. REPAIRED IAW ECRA 5310-03851 REVISION A.
- [SDR CALA0001229](https://openairdocs.org/sdr/CALA0001229.md): Floorbeam · corroded · Aug 7, 2000 · N70353 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT NUT CLIPS, BS 986.5. REPAIRED IAW ECRA 5310-03851.
- [SDR CALA0001214](https://openairdocs.org/sdr/CALA0001214.md): Angle · corroded · Aug 6, 2000 · N70353 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ANGLE CORRODED AT RT SIDE OF FUSELAGE, BS 251.6, BL 0. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-00.
- [SDR CALA0001231](https://openairdocs.org/sdr/CALA0001231.md): Stiffener · cracked · Aug 4, 2000 · N70353 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND VERTICAL STIFFENERS CRACKED THROUGH (2 INCH CRACK) IN MLG W/W AT BS 664, RBL 6 AND LBL 6. THE VERTICAL STIFFENERS WERE REMOVED AND REPLACED IAW SRM 51-40-01 AND 51-10-02.
- [SDR CALA0001199](https://openairdocs.org/sdr/CALA0001199.md): Cargo Track · corroded · Aug 4, 2000 · N70353 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND CORROSION AROUND SCREW HOLES ON TIE DOWN RAIL AT BS 727 - 947.5, RBL 13. REPAIRED IAW SRM 53-00-53, PAGE 205, FIGURE 205.
- [SDR CALA0001163](https://openairdocs.org/sdr/CALA0001163.md): Seat Track · corroded · Jul 26, 2000 · N70353 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT I/B SEAT TRACK CORRODED AT BS 907 - 935, AFT GALLEY FLOOR AREA. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52.
- [SDR CALA0001153](https://openairdocs.org/sdr/CALA0001153.md): Seat Track · corroded · Jul 25, 2000 · N70353 · Boeing 7373T0 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED IN AFT GALLEY MOUNT AREA AT BS 917. THE TRACK WAS REMOVED AND REPLACED IAW SRM 53-00-52, PAGE 213.
- [SDR CALA0001152](https://openairdocs.org/sdr/CALA0001152.md): Skin · cracked · Jul 25, 2000 · N70353 · Boeing 7373T0 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN LT ENGINE PYLON TOP CUTOUT PANEL NR 5727. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5430-01230. A DIP WAS INITIATED TO REINSPECT THE SKIN AND DOUBLER FOR CRACK GROWTH EVERY 150 FLIGHT CYCLES UNTIL TIP OF CRACK REACHES PRODUC
- [SDR CALA0001143](https://openairdocs.org/sdr/CALA0001143.md): Floorbeam · corroded · Jul 23, 2000 · N70353 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM UPPER T-CHORD CORRODED AT STA 344, LBL 49 TO RBL 2. THE UPPER T-CHORD WAS REMOVED AND REPLACED IAW SRM 53-10-51, PAGE 222.
- [SDR CALA0000779](https://openairdocs.org/sdr/CALA0000779.md): Battery Pack · inoperative · May 30, 2000 · N70353 · Boeing 7373T0 · Emergency Lighting
  > INSPECTION FOUND LT OVERWING EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED AND REPLACED. OPERATION OF THE LIGHT WAS RESTORED.
- [SDR CALA9701526](https://openairdocs.org/sdr/CALA9701526.md): Skin · delaminated · Oct 30, 1997 · N70353 · Boeing 7373T0 · Trailing Edge Flaps
  > INSPECTION FOUND RT OUTBOARD FLAP TRAILING EDGE INBOARD SIDE DELAMINATED. THE FLAP WAS REPAIRED IAW ECRA 5750-02806.
- [SDR CALA9601034](https://openairdocs.org/sdr/CALA9601034.md): Floor Beam · corroded · Jun 21, 1996 · N70353 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOOR BEAM CORRODED AT SCREW HOLES, STA 344. THE CORRODED AREA WAS CUT OUT AND A FLOOR BEAM WAS INSTALLED IAW SRM 53-10-51.
- [SDR CALA9601033](https://openairdocs.org/sdr/CALA9601033.md): Floor Beam · corroded · Jun 21, 1996 · N70353 · Boeing 7373T0 · Fuselage Main, Floor Beam
  > INSPECTION FOUND AFT CABIN FLOOR BEAM CHORD AT STA 947.5 CORRODED AROUND SCREW HOLES NEAR CENTERLINE. THE CHORD WAS REMOVED AND REPLACED IAW SRM 53-00-51.
- [SDR CALA9601032](https://openairdocs.org/sdr/CALA9601032.md): Intercostal · corroded · Jun 21, 1996 · N70353 · Boeing 7373T0 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND THE RIGHT AFT LAV WALL FLOOR SUPPORT INTERCOSTAL CORRODED AROUND SCREW HOLES AT STA 993. A FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-02 AND 5310-03298.

Next page: https://openairdocs.org/deregistered/N70353-2012-08-23/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 = 'N70353' AND deregistration_id = 'N70353-2012-08-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N70353-2012-08-23/reports

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