# Service difficulty reports: N624DH, cancelled May 9, 2000

A list on [N624DH, cancelled May 9, 2000](https://openairdocs.org/deregistered/N624DH-2000-05-09.md).

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

- [SDR MZZA99185](https://openairdocs.org/sdr/MZZA99185.md): Antenna · failed · Oct 5, 1999 · N624DH · Boeing 727264 · Landing Gear Door Actuator
  > FLT 891 - MNL - RADAR FAILED IN FLIGHT CRWE RESET CIRCUIT BREAKERS IN FLIGHT, NO EFFECT. INDICATOR SHOW MANY SMALL DOTS ON SCREEN. DUMP FUEL AND AIR RETURN TO MANILLA. GOT GOOD TEST PATTERN ON THE GROUND. MAINTENANCE T/S SYSTEM AND FOUND RADAR ANTENNA AT F
- [SDR MZZA97266](https://openairdocs.org/sdr/MZZA97266.md): Floor Panel · corroded · Oct 29, 1997 · N624DH · Boeing 727264 · Fuselage Floor Panel
  > HKG - ON WALK AROUND DISCOVER CORROSION AT STATION 440 BETWEEN STRINGER STRINGER 28R AND STRINGER 27R. OPENED FORWARD CARGO FLOOR PANEL AND INSEPCTED DAMAGED AREA. THERE IS NO DAMAGE TO THE STRINGER AND FRAME WEB ASSEMBLY. CUTOUT DAMAGED AREA 2.4 INBY BY 2.
- [SDR MZZA97956](https://openairdocs.org/sdr/MZZA97956.md): Pivot Pin · migrated · Aug 22, 1997 · N624DH · Boeing 727264 · Passenger/Crew Doors
  > MNL - FLT 879 - L/P: 7964981/4188932 - MAIN ENTRY DOOR (L-1) LOWER HINGE COVER ASSY LEAKING DURING PRESSURIZATION IN CLIMB. AIRCRAFT AIR RETURN TO STATION. UPON INSPECTION BY MAINTENANCE, FOUND THAT THE L-1 DOOR HINGE COVER PIVOT PIN MIGRATED ALLOWING HING
- [SDR MZZA97155](https://openairdocs.org/sdr/MZZA97155.md): Skin · corrosion · Jun 28, 1997 · N624DH · Boeing 727264 · Trailing Edge Flaps
  > KUL - S-CHECK. NRC: 861510 - RT INBOARD AFT FLAP UPPER SIDE HAS CHIPPED PAINT AND SURFACE CORROSION ALONG THE ENTIRE SPAN. CORROSION REMOVED - DIMENSIONS 36 INCHES BY.50 INCH BY 0.002 INCH WITHIN LIMITS IAW SRM 57-50-1. AREA ALODINED, PRIMED, AND REPAINTE
- [SDR MZZA97151](https://openairdocs.org/sdr/MZZA97151.md): Skin · delamination · Jun 28, 1997 · N624DH · Boeing 727264 · Trailing Edge Flaps
  > KUL - S-CHECK. NRC: 851461 - RIGHT WING OUTBOARD MID-FLAP, T/E HAS DELAMINATION 12 INCHES INBOARD AND 6 INCHES OUTBOARD OF THE AFT FLAP INBOARD TRACK.
- [SDR MZZA97181](https://openairdocs.org/sdr/MZZA97181.md): Bracket · cracked · Jun 2, 1997 · N624DH · Boeing 727264 · Fuselage Miscellaneous Structure
  > KUL - S-CHECK. NRC: 851665 - RIGHT RAM AIR INTAKE FAIRING SUPPORT BRACKET CRACKED AT SCREW ATTACHMENT. REMOVED CRACK BRACKET AND FABRICATED IAW SRM 53-50-1. (X)
- [SDR MZZA97176](https://openairdocs.org/sdr/MZZA97176.md): Skin · gouged · Jun 2, 1997 · N624DH · Boeing 727264 · Fuselage Main, Plate/Skin
  > KUL - S-CHECK. NRC: 851120 - GOUGE ON SKIN JUST BELOW MAIN CARGO SILL APPROXIMATELY 1.50 INCHES. GOUGE SMOOTHED AND FOUND WITHIN LIMITS IAW SRM 5-40-1. TREATED WITH ALODINE AND PRIMER. (X)
- [SDR MZZA97175](https://openairdocs.org/sdr/MZZA97175.md): Skin · misrepaired · Jun 2, 1997 · N624DH · Boeing 727264 · Fuselage Main, Plate/Skin
  > KUL - S-CHECK. NRC: 851117 - EVALUATED PATCH REPAIR BETWEEN STA 1050 - STA 1070, S26R. PATCH REPAIR EVALUATED, REPAIR CARRIED OUT. FABRICATED REPAIR PARTS. ALODINED AND PRIMED IAW SRM 53-30-3. (X)
- [SDR MZZA97174](https://openairdocs.org/sdr/MZZA97174.md): Skin · dented · Jun 2, 1997 · N624DH · Boeing 727264 · Fuselage Main, Plate/Skin
  > KUL - S-CHECK. NRC: 851541 - RIGHT FUSELAGE AT STA 700 HAS DENT OF 1 INCH. REQUIRED REPAIRS DUE TO OIL CANNING. REPAIRED AND FABRICATED FUSELAGE REPAIR PART IAW SRM 53-30-3. TREATED WITH ALODINE AND PRIMER. (X)
- [SDR MZZA97171](https://openairdocs.org/sdr/MZZA97171.md): Hinge · worn · May 28, 1997 · N624DH · Boeing 727264 · Elevator, Tab Structure
  > KUL - S-CHECK. NRC: 851582 - LEFT HAND ELEVATOR TAB HAS EXCESSIVE PLAY. REMOVED, REPAIRED HINGES, AND REINSTALLED ELEVATOR TAB IAW MM 27-30-11. FUNCTIONAL CHECK GOOD. (X)
- [SDR MZZA97160](https://openairdocs.org/sdr/MZZA97160.md): Skin · corrosion · May 28, 1997 · N624DH · Boeing 727264 · Wing, Plate/Skin
  > KUL - S-CHECK. NRC: 851550 - LEFT WING FORWARD SPAR UPPER CHORD (COVER STRIP) AT OUTBOARD TIP OF NR 1 SLAT HAS SURFACE CORROSION AND JUST OUTBOARD OF NR 2 SLAT OUTBOARD BAYONET. CORROSION REMOVED, DIMENSIONS, 2 INCHES BY.50 INCH BY 0.002 INCH WITHIN LIMITS
- [SDR MZZA97159](https://openairdocs.org/sdr/MZZA97159.md): Skin · corrosion · May 28, 1997 · N624DH · Boeing 727264 · Wing, Plate/Skin
  > KUL - LEFT WING TOP SKIN 4 INCHES AFT OF FORWARD SPAR BEHIND NR 1 SLAT TIP HAS SURFACE CORROSION. CORROSION REMOVED DIMENSION 2 INCH BY 1 INCH BY 0.002 INCH WITHIN LIMITS IAW SRM 57-30-1 AREA ALODONE, PRIMED, AND REPAINTED IAW CONTL SPEC 5100DD485. (X)
- [SDR MZZA97158](https://openairdocs.org/sdr/MZZA97158.md): Skin · corroded · May 28, 1997 · N624DH · Boeing 727264 · Wing, Plate/Skin
  > KUL - NUMEROUS AREAS OF CHIPPED PAINT AND SURFACE CORROSION RT WING UPPER SURFACE AFT OF CORROSION AND JUST OUTBOARD OF NR 2 SLAT OUTBOARD BAYONET. CORROSION REMOVED DIMENSION 2 INCH BY.50 INCH BY 0.002 INCH WITHIN LIMITS IAW SRM 57-30-1 AREA ALODINE REAR SP
- [SDR MZZA97157](https://openairdocs.org/sdr/MZZA97157.md): Skin · corrosion · May 28, 1997 · N624DH · Boeing 727264 · Fuselage Main, Plate/Skin
  > KUL - S-CHECK. NRC: 851123 - LEFT COCKPIT WINDOW FRAME AND AROUND THE AREA HAS MANY RUSTY SCREWS AND REQUIRE REPAINTING. CORROSION REMOVED, 0.050 INCH. FOUND WITHIN LIMITS. AREA ALODINED AND PAINTED IAW SRM 51-10-1. 9X)
- [SDR MZZA97156](https://openairdocs.org/sdr/MZZA97156.md): Skin · corrosion · May 28, 1997 · N624DH · Boeing 727264 · Trailing Edge Flaps
  > KUL - S-CHECK. NRC: 851509 - RIGHT INBOARD MID-FLAP UPPER SIDE HAS AREAS OF CHIPPED PAINT AND SURFACE CORROSION ALONG THE ENTIRE SPAN. 2 X AREAS OF CORROSION REMOVED. DIMENSIONS T INCHES BY 1 INCH BY 0.002 INCH AND 2 INCHES BY 1 INCH BY 0.002 INCH WITHIN L
- [SDR MZZA97152](https://openairdocs.org/sdr/MZZA97152.md): Support · corrosion · May 28, 1997 · N624DH · Boeing 727264 · Fuselage Miscellaneous Structure
  > KUL - S-CHECK. NRC: 851276 - STA 960C, 950D CENTER FLOOR SUPPORT HAS CORROSION AROUND ANCHOR NUT HOLE. FABRICATED FLOOR SUPPORT. ALODINED AND PRIMED IAW SRM 51-40-3 AND SRM 51-30-2. (X)
- [SDR MZZA97150](https://openairdocs.org/sdr/MZZA97150.md): Skin · cracked · May 28, 1997 · N624DH · Boeing 727264 · Spoilers
  > KUL - RT WING TOPSIDE JUST FORWARD OF NR 12 SPOILER HAS A 1 INCH CRACK ON THE SKIN ATTACHED TO THE UPPER CHORD OF AFT SPAR. FABRICATED REPAIR PER SRM 57-30-4. INSTALLED REPAIR PER SRM 51-30-2. (X)
- [SDR MZZA97149](https://openairdocs.org/sdr/MZZA97149.md): Skin · delaminated · May 28, 1997 · N624DH · Boeing 727264 · Spoilers
  > NR 1 SPOILER DELAMINATED TOP SIDE INBOARD END APPROXIMATELY 3 INCHES BY 4 INCHES. REMOVED NR 10 SPOILER REPAIRED PER SRM 57-40-6 AND REPLACED PER 27-61-41. OPERATIONAL CHECK GOOD. (X)
- [SDR MZZA624DH](https://openairdocs.org/sdr/MZZA624DH.md): Hinges · worn · May 28, 1997 · N624DH · Boeing 727264 · Elevator, Tab Structure
  > KUL - S-CHECK. NRC: 851581 - RIGHT HAND ELEVATOR TAB HAS EXCESSIVE PLAY. REMOVED TAB IAW MM 27-30-11. REPAIRED HINGES IAW 27-30-02. REINSTALLED TAB IAW 27-30-11. FUNCTIONAL CHECK GOOD. (X)
- [SDR MZZA97068](https://openairdocs.org/sdr/MZZA97068.md): Mod Valve · failed · Apr 16, 1997 · N624DH · Boeing 727264 · Pneumatic Distribution System
  > MNL - FLT 876 - DURING CRUISE GOT A BLEED TRIP ON NR 3 ENGINE, SELECTED NR 2 BLEED SOURCE. TRIED TO RESET NR 3 DUCT PRESSURE, STILL PLUS 100 PSI. AFTER SELECTING NR 2 BLEED GOT AFT BODY OVERHEAT LIGHT. AIR RETURN. REMOVED AND REPLACED 13TH STAGE MOD VALVE
- [SDR MZZA96063](https://openairdocs.org/sdr/MZZA96063.md): Fire Detector · failed · Aug 9, 1996 · N624DH · Boeing 727264 · Fire Detection
  > MNL - FLT 880 - AT CRUISE JUST PRIOR TO DESCENT, THE APU FIRE LIGHT AND ALARM WENT OFF. FIRE HANDLE WAS PULLED AND DISCHARGE BUTTON PUSHED. LIGHT REMAINED ILLUMINATED. REMOVED APU SHROUD AND CHECKED APU FOR EVIDENCE OF FIRE, NONE FOUND. SUSPECT FALSE WARNI
- [SDR MZZA96061](https://openairdocs.org/sdr/MZZA96061.md): Fire Detection · failed · Aug 1, 1996 · N624DH · Boeing 727264 · Fire Detection
  > MNL - FLT 879 - ON GROUND IN MNL, CREW STARTED APU. AFTER APPROXIMATELY 8 MINUTES RECEIVED APU FIRE WARNING. CREW C/W EMERGENCY PROCEDURES TO PULL FIRE HANDLE AND FIRE BOTTLE. PER CREW COMMENTS, APU GENERATOR OPERATED NORMALLY - 116 VAC 403 CYC. FREQUENCY

## 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 = 'N624DH' AND deregistration_id = 'N624DH-2000-05-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N624DH-2000-05-09/reports

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