# Service difficulty reports: N70542, cancelled Jul 14, 2000

A list on [N70542, cancelled Jul 14, 2000](https://openairdocs.org/deregistered/N70542-2000-07-14.md).

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

- [SDR CALA9801853](https://openairdocs.org/sdr/CALA9801853.md): Vane · gouged · Sep 22, 1998 · N70542 · Doug DC932 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING UPPER MOVEABLE VANE LEADING EDGE GOUGED. A REPAIR WAS INSTALLED IAW SRM 57-01, FIGURE 1, 51-10-4, 51-10-3, 51-30-2, AND 51-10-2.
- [SDR CALA9801836](https://openairdocs.org/sdr/CALA9801836.md): Skin · dented · Sep 19, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 160, LONGERON 26R. THE DENTED AREA WAS CUT OUT IAW ECRA 5331-01030. DOUBLERS AND FILLER WERE INSTALLED IAW ECRA 5331-01030, SRM 51-10-3 AND 51-30-2.
- [SDR CALA9801813](https://openairdocs.org/sdr/CALA9801813.md): Skin · lightning strike · Sep 17, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LIGHTNING STRIKE DAMAGE IN LT FUSELAGE SKIN AT STRINGER 25L, STA 246. THE DAMAGED AREA WAS CUT OUT, DOUBLER AND FILLER WERE INSTALLED IAW ECRA 5331-01031.
- [SDR CALA9801812](https://openairdocs.org/sdr/CALA9801812.md): Seat Track · corroded · Sep 17, 1998 · N70542 · Doug DC932 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND FORWARD COCKPIT CO-PILOT'S SEAT TRACK CORRODED AT STA 203.9. THE SEAT TRACK WAS REMOVED AND REPLACED IAW MM 53-40-1.
- [SDR CALA9801778](https://openairdocs.org/sdr/CALA9801778.md): Skin · cracked · Sep 15, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND TOP OF FUSELAGE AFT ADF LOOP ANTENNA MOUNTING SURFACE EXTERNAL SKIN CRACKED AT RT CENTER MOUNT HOLE, STA 259 LONGERON 1R, BL 0 AND AT RT MOUNT HOLE, STA 265, LONGERON 1R, BL 0. BOTH CRACKS WERE.375 INCH LONG. THE CRACKED AREAS OF SKIN WERE
- [SDR CALA9801752](https://openairdocs.org/sdr/CALA9801752.md): Fairing · delaminated · Sep 14, 1998 · N70542 · Doug DC932 · Horizontal Stabilizer Structure
  > INSPECTION FOUND LT HORIZONTAL STABILIZER UPPER FAIRING DELAMINATED FROM AFT ATTACH POINT FORWARD. REMOVED PAN ON LOWER SURFACE AND REMOVED DELAMINATED HONEYCOMB. NEW HONEYCOMB WAS BONDED IN LOWER PAN AND THEN PAN WAS INSTALLED ON FAIRING AND BONDED IAW SRM 5
- [SDR CALA9801751](https://openairdocs.org/sdr/CALA9801751.md): Fairing · delaminated · Sep 14, 1998 · N70542 · Doug DC932 · Horizontal Stabilizer Structure
  > INSPECTION FOUND RT LOWER HORIZONTAL STABILIZER FAIRING DELAMINATED AT FWD END. THE DELAMINATED HONEYCOMB CORE, DOUBLER, AND PLATE WERE REMOVED. BONDED DOUBLER WITH HONEYCOMB CORE AND PLATE TO SKIN FAIRING IAW ECRA 5510-01317, SRM 51-70-2, 51-30-2.
- [SDR CALA9801750](https://openairdocs.org/sdr/CALA9801750.md): Frame · gouged · Sep 14, 1998 · N70542 · Doug DC932 · Fuselage Main, Frame
  > INSPECTION FOUND FRAME GOUGED AT STA 332, LONGERON 29L TO 30. A SPLICE AND PLATE REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 2A AND 51-10-2A.
- [SDR CALA9801749](https://openairdocs.org/sdr/CALA9801749.md): Fitting · gouged · Sep 14, 1998 · N70542 · Doug DC932 · Trailing Edge Flaps
  > INSPECTION FOUND FLAP FITTING GOUGED AT AFT END OF LT WING AFT MOVEABLE VANE INBOARD TRACK STA XFLS 65.612 TO 69.125. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA9801748](https://openairdocs.org/sdr/CALA9801748.md): Web · cracked · Sep 14, 1998 · N70542 · Doug DC932 · Nacelle/Pylon Structure
  > INSPECTION FOUND THREE 2 INCH CRACKS ON NR 1 ENGINE PYLON INTERNAL WEB AT STA 1065. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 54-01, FIGURE 2.
- [SDR CALA9801747](https://openairdocs.org/sdr/CALA9801747.md): Tab · delaminated · Sep 14, 1998 · N70542 · Doug DC932 · Elevator, Tab Structure
  > INSPECTION FOUND TWO AREAS OF DELAMINATION ON UPPER SURFACE OF LT ELEVATOR CONTROL TAB BETWEEN THIRD AND OUTBOARD HINGES. THE DELAMINATED AREAS WERE TRIMMED OUT AND FILLER AND DOUBLER WERE INSTALLED IAW SRM 51-70-2.
- [SDR CALA9801746](https://openairdocs.org/sdr/CALA9801746.md): Skin · cracked · Sep 14, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 1 INCH CRACK IN FUSELAGE SKIN AT STA 950, THREE INCHES BELOW LONGERON 14L. THE CRACKED AREA WAS REMOVED IAW SRM 53-04, FIGURE 38. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 53-04, FIGURE 38.
- [SDR CALA9801686](https://openairdocs.org/sdr/CALA9801686.md): Bracket · corroded · Sep 9, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SUPPORT BRACKET CORRODED AT STA 917, STRINGER 28L. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-10-3, 51-10-4, AND 51-30-1.
- [SDR CALA9801685](https://openairdocs.org/sdr/CALA9801685.md): Hat Channel · cracked · Sep 9, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3 CRACK IN HAT CHANNEL AT FLOORBOARD PANEL, LT SIDE, STA 756. A NEW HAT CHANNEL SECTION WAS INSTALLED IAW SRM 53-05, PAGE 1 AND 51-30-2.
- [SDR CALA9801659](https://openairdocs.org/sdr/CALA9801659.md): Fairing · cracked · Sep 8, 1998 · N70542 · Doug DC932 · Horizontal Stabilizer Structure
  > INSPECTION FOUND A 4.5 INCH CRACK IN LOWER AFT END OF RT HORIZONTAL STABILIZER LOWER FAIRING. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW SRM 55-11-0 FIGURE 7, 55-01, FIGURE 2, 51-10-3, AND 51-30-2.
- [SDR CALA9801654](https://openairdocs.org/sdr/CALA9801654.md): Doubler · cracked · Sep 8, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TWO 1 INCH CRACKS IN DOUBLER AT STA 945, LONGERON 14R. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 53-03, FIGURE 28.
- [SDR CALA9801653](https://openairdocs.org/sdr/CALA9801653.md): Floor · cracked · Sep 8, 1998 · N70542 · Doug DC932 · Fuselage Floor Panel
  > INSPECTION FOUND 1 INCH CRACKS AT CLIP NUT HOLES IN FLOOR PANEL NR 47 FORWAD OF STA 756. A NEW FLOOR PANEL WAS INSTALLED IAW SRM 53-21, 51-30-2, AND 53-05, FIGURE 1.
- [SDR CALA9801636](https://openairdocs.org/sdr/CALA9801636.md): Frame · cracked · Sep 4, 1998 · N70542 · Doug DC932 · Fuselage Main, Frame
  > INSPECTION FOUND A 1 INCH CRACK AT UPPER MOUNT HOLE OF FRAME AT STA 980, LONGERON 16R. THE CRACKED AREA WAS REMOVED. A REPAIR WAS INSTALLED IAW SRM 51-30-1.
- [SDR CALA9801621](https://openairdocs.org/sdr/CALA9801621.md): Web · corroded · Sep 2, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND WEB CORRODED AT FORWARD CARGO DOOR, STA 370, STRINGER 28R. A DOUBLER REPAIR WAS INSTALLED IAW SRM 53-01, FIGURE 2.
- [SDR CALA9801620](https://openairdocs.org/sdr/CALA9801620.md): Skin · cracked · Sep 2, 1998 · N70542 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.25 INCH CRACK AT FASTENER IN TAIL SECTION SKIN AT STA 1062 APPROXIMATELY FOUR INCHES BELOW LONGERON 15L. THE FASTENER WAS REMOVED IAW SRM 51-30-2 AND THE CRACKED AREA WAS CUT OUT IAW SRM 53-04, FIGURE 28. A DOUBLER REPAIR WAS INSTALLED IA
- [SDR CALA9801619](https://openairdocs.org/sdr/CALA9801619.md): Bulkhead Strap · cracked · Sep 2, 1998 · N70542 · Doug DC932 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 1 INCH CRACK IN LOWER SUPPORT STRAP OF FORWARD BULKHEAD WALL IN AFT PIT, FS 737. THE SUPPORT STRAP WAS REMOVED AND A NEW SUPPORT STRAP WAS INSTALLED IAW SRM 51-10-2, 51-10-4, AND 51-10-3.
- [SDR CALA9801610](https://openairdocs.org/sdr/CALA9801610.md): Longeron · cracked · Sep 1, 1998 · N70542 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 2 INCH CRACK IN LONGERON 17L AT ANGLE MOUNT, STA 965. THE CRACKED SECTION OF LONGERON WAS CUT OUT IAW SRM 53-02, FIGURE 18. A NEW LONGERON SECTION AND SPLICE WERE INSTALLED IAW SRM 51-30-5.
- [SDR CALA9801586](https://openairdocs.org/sdr/CALA9801586.md): Clip · cracked · Aug 28, 1998 · N70542 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH CRACK IN SHEAR TIE CLIP AT LT AFT CABIN STA 965 UNDER LONGERON 13L. THE CRACK WAS REMOVED AND A CLIP REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 28.
- [SDR CALA9801585](https://openairdocs.org/sdr/CALA9801585.md): Skin · cracked · Aug 28, 1998 · N70542 · Doug DC932 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD CARGO DOOR SKIN AT LOWER AFT CORNER. THE CRACKED AREA WAS CUT OUT AND A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW SRM 52-01, FIGURE 4.
- [SDR CALA9601153](https://openairdocs.org/sdr/CALA9601153.md): Cables · out of adjust · Aug 9, 1996 · N70542 · Doug DC932 · Aerodynamic Fairings
  > TAILCONE RELEASE USING INTERIOR HANDLE PULLED LOW AT 15 POUNDS. THE TAILCONE CABLES WERE ADJUSTED IAW MM 53-50-00.
- [SDR CALA9601194](https://openairdocs.org/sdr/CALA9601194.md): Skin · corroded · Aug 6, 1996 · N70542 · Doug DC932 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 594, LONGERON 17R. THE CORROSION WAS REMOVED AND AN INTERNAL DOUBLER WAS INSTALLED IAW ECRA 5330-02427.
- [SDR CALA9601195](https://openairdocs.org/sdr/CALA9601195.md): Skin · cracked · Aug 1, 1996 · N70542 · Doug DC932 · Elevator, Plate/Skin
  > INSPECTION FOUND A 5 INCH CRACK IN RT ELEVATOR LOWER SKIN AT STA XHS 86.0. AN EXTERNAL DOUBLER WAS INSTALLED IAW ECRA 5530-01174 AND SRM 55-03, FIGURE 13.
- [SDR CALA9601225](https://openairdocs.org/sdr/CALA9601225.md): Frame · cracked · Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, Frame
  > INSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 446, LONGERON 5L. THE CRACKS WERE 3 LONG. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4.
- [SDR CALA9601224](https://openairdocs.org/sdr/CALA9601224.md): Frame · cracked · Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, Frame
  > INSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 446, LONGERON 5R. THE CRACKS WERE 2.5 LONG. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4.
- [SDR CALA9601223](https://openairdocs.org/sdr/CALA9601223.md): Frame · cracked · Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, Frame
  > INSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 427, LONGERON 5R. THE CRACKS WERE 1.5 LONG. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4.
- [SDR CALA9601222](https://openairdocs.org/sdr/CALA9601222.md): Frame · cracked · Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, Frame
  > INSPECTION FOUND BELTFRAME CRACKED IN TWO PLACES AT STA 427, LONGERON 5L. THE CRACKS WERE 3.5 LONG. THE CRACKED SECTION OF FRAME WAS CUT OUT AND A REPAIR WAS INSTALLED IAW SRM 53-03, FIGURE 4.
- [SDR CALA9601198](https://openairdocs.org/sdr/CALA9601198.md): Longeron · cracked · Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 5R CRACKED AT STA 737. A NEW SECTION OF LONGERON WAS SPLICED IN IAW SRM 53-02, FIGURE 2.
- [SDR CALA9601192](https://openairdocs.org/sdr/CALA9601192.md): Longeron · cracked · Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 3L CRACKED AT STA 160. THE CRACKED SECTION OF LONGERON WAS REMOVED AND A NEW SECTION WAS SPLICED IN IAW SRM 53-02, FIGURE 2.
- [SDR CALA9601191](https://openairdocs.org/sdr/CALA9601191.md): Longeron · cracked · Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 4L CRACKED AT STA 200. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 2.
- [SDR CALA9601190](https://openairdocs.org/sdr/CALA9601190.md): Longeron · cracked · Jul 30, 1996 · N70542 · Doug DC932 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND LONGERON 4L CRACKED AT STA 160. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 53-02, FIGURE 2.
- [SDR CALA9601144](https://openairdocs.org/sdr/CALA9601144.md): Spar · corroded · Jul 30, 1996 · N70542 · Doug DC932 · Horizontal Stabilizer, Spar/Rib
  > INSPECTION FOUND CORROSION ON UPPER SPAR CAP OF LT HORIZONTAL STABILIZER FORWARD SIDE OF REAR SPAR AT STA XHS 95. THE CORRODED SECTION OF SPAR CAP WAS CUT OUT AND A NEW SECTION WAS SPLICED IN IAW SRM 55-02, PAGES 85 TO 87.
- [SDR CALA9601114](https://openairdocs.org/sdr/CALA9601114.md): Spar Nut · cracked · Jul 30, 1996 · N70542 · Doug DC932 · Elevator, Spar/Rib
  > INSPECTION FOUND, LT ELEVATOR MOST OUTBOARD BOTTOM NUT ON SPAR CRACKED. THE NUT WAS REMOVED AND REPLACED PER MM 20-16-0.
- [SDR CALA9601227](https://openairdocs.org/sdr/CALA9601227.md): Bulkhead Angle · cracked · Jul 29, 1996 · N70542 · Doug DC932 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 1 INCH CRACK IN FRONT SPAR TO PRESSURE BULKHEAD ATTACH ANGLE AT STA 598, LONGERON 24L. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0.
- [SDR CALA9601226](https://openairdocs.org/sdr/CALA9601226.md): Bulkhead Angle · cracked · Jul 29, 1996 · N70542 · Doug DC932 · Fuselage Main, Bulkhead
  > INSPECTION FOUND A 3 INCH CRACK IN FRONT SPAR TO PRESSURE BULKHEAD ATTACH ANGLE AT STA 598, LONGERON 24R. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-0.
- [SDR CALA9601202](https://openairdocs.org/sdr/CALA9601202.md): Frame · cracked · Jul 28, 1996 · N70542 · Doug DC932 · Fuselage Main, Frame
  > INSPECTION FOUND A CRACK IN FRAME JUST FORWARD OF RUDDER TRIM MOUNT AT TAIL COMPARTMENT STA 1143. A NEW ANGLE WAS INSTALLED ON FRAME IAW SRM 51-10-4.
- [SDR CALA9601193](https://openairdocs.org/sdr/CALA9601193.md): Support · cracked · Jul 28, 1996 · N70542 · Doug DC932 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK ON FLOOR SUPPORT IN FORWARD CARGO COMPARTMENT AT STA 484, LONGERON 24R. A DOUBLER WAS INSTALLED IAW ECRA 5320C01263.
- [SDR CALA9601201](https://openairdocs.org/sdr/CALA9601201.md): Rib · cracked · Jul 27, 1996 · N70542 · Doug DC932 · Wing, Rib/Bulkhead
  > INSPECTION FOUND A 1 INCH CRACK IN WING LEADING EDGE RIB AT NR 1 SLAT TRACK. THE RIB WAS REPAIRED IAW ECRA 5710-01751.
- [SDR CALA9601200](https://openairdocs.org/sdr/CALA9601200.md): Beam · cracked · Jul 27, 1996 · N70542 · Doug DC932 · Cargo/Baggage Doors
  > INSPECTION FOUND A.75 INCH CRACK IN FORWARD CARGO COMPARTMENT DOOR BEAM AT LOWER FORWARD STOP. A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 51-30-3.
- [SDR CALA9601199](https://openairdocs.org/sdr/CALA9601199.md): Fitting · cracked · Jul 27, 1996 · N70542 · Doug DC932 · Cargo/Baggage Doors
  > INSPECTION FOUND A.375 INCH CRACK IN AFT CARGO COMPARTMENT DOOR FITTING INSIDE DOOR AT BOTTOM CENTER STOP. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA9601197](https://openairdocs.org/sdr/CALA9601197.md): Beam · cracked · Jul 27, 1996 · N70542 · Doug DC932 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1.5 INCH CRACK IN AFT CARGO COMPARTMENT DOOR BEAM AT UPPER FORWARD STOP. THE BEAM WAS REMOVED AND REPLACED IAW SRM 52-01, FIGURE 1.
- [SDR CALA9601196](https://openairdocs.org/sdr/CALA9601196.md): Beam · cracked · Jul 27, 1996 · N70542 · Doug DC932 · Cargo/Baggage Doors
  > INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD CARGO COMPARTMENT DOOR BEAM AT UPPER FORWARD STOP. A REPAIR WAS DONE IAW SRM 51-30-2.
- [SDR CAL950783](https://openairdocs.org/sdr/CAL950783.md): Fuel Coupling · leaking · Sep 2, 1995 · N70542 · Doug DC932 · Aircraft Fuel Distribution System
  > IAH - FLT 1230 - THE LEFT MAIN FUEL QUANTITY BEGAN TO DECREASE AS FUEL WAS TRANSFERRED FROM CENTER TANK AFTER TAKEOFF FROM IAH. THE LEFT FUEL QUANTITY STEADILY AND RAPIDLY DECREASED. THE CROSS-FEED WAS OPENED IN AN ATTEMPT TO BURN RT MAIN FUEL, BUT THE LT FU

## 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 = 'N70542' AND deregistration_id = 'N70542-2000-07-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N70542-2000-07-14/reports

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