# Service difficulty reports: N14788, cancelled Aug 29, 2000

A list on [N14788, cancelled Aug 29, 2000](https://openairdocs.org/deregistered/N14788-2000-08-29.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 4 · 200 reports

- [SDR CALA9901504](https://openairdocs.org/sdr/CALA9901504.md): Battery · discharged · Nov 16, 1999 · N14788 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND THE RT CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. THE BATTERY PACK WAS REMOVED, CHARGED, AND REINSTALLED. OPERATION CHECKED GOOD IAW MM 33-50-22, PAGE 401.
- [SDR CALA9901503](https://openairdocs.org/sdr/CALA9901503.md): Battery · discharged · Nov 16, 1999 · N14788 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND R-2 DOOR EXIT IDENTIFIER INOPERATIVE. THE BATTERY PACK WAS REMOVED, CHARGED AND REINSTALLED. OPERATION CHECKED GOOD IAW MM 33-50-22, PAGE 401.
- [SDR CALA9901502](https://openairdocs.org/sdr/CALA9901502.md): Batteries · discharged · Nov 16, 1999 · N14788 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND SELF CONTAINED FIXED EMERGENCY LIGHT INOPERATIVE IN FORWARD CABIN. THE LIGHT ASSEMBLY WAS REMOVED, THE BATTERIES WERE REPLACED, AND THE LIGHT WAS REINSTALLED. OPERATION CHECKED GOOD IAW MM 33-50-101, PAGE 203.
- [SDR CALA9901500](https://openairdocs.org/sdr/CALA9901500.md): Skin · delaminated · Nov 15, 1999 · N14788 · Boeing 727232 · Spoilers
  > INSPECTION FOUND THE NR 8 SPOILER DELAMINATED. THE NR 8 SPOILER WAS REPLACED IAW MM 27-62-1.
- [SDR CALA9900463](https://openairdocs.org/sdr/CALA9900463.md): Power Supply · inoperable · May 1, 1999 · N14788 · Boeing 727232 · Emergency Lighting
  > IAH - TWO OVERWING EMERGENCY LIGHTS AND ONE EMERGENCY LIGHT AFT OF FLAPS LEFT SIDE OF FUSELAGE INOPERABLE. FOUND M654, M954, AND M955 POWER SUPPLIES BAD. REPLACED POWER SUPPLIES AND LIGHT ASSEMBLIES L878, L877, AND L822. EMERGENCY LIGHTS OPS CHECK NORMAL.
- [SDR CALA9900198](https://openairdocs.org/sdr/CALA9900198.md): Wire · broken · Feb 28, 1999 · N14788 · Boeing 727232 · Light System Wiring
  > INSPECTION FOUND THE LAST FIVE AISLE PATH LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE FOUND A BROKEN WIRE AT AFT BATTERY PACK. THE WIRE WAS REPAIRED AND OPERATION CHECKED GOOD.
- [SDR CALA9801921](https://openairdocs.org/sdr/CALA9801921.md): Connector · shorted · Oct 7, 1998 · N14788 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND LT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND THE CANNON PLUG SHORTED AT POWER SUPPLY. THE PLUG WAS REPLACED AND EXIT LIGHT OPERATION WAS RESTORED.
- [SDR CALA9801900](https://openairdocs.org/sdr/CALA9801900.md): Web · cracked · Oct 1, 1998 · N14788 · Boeing 727232 · Landing Gear Doors
  > INSPECTION FOUND A 1 INCH CRACK IN RT MLG FLYING DOOR WEB FORWARD OF AFT HINGE FITTING. THE HINGE WEB WAS REMOVED IAW SRM 51-30-2. A NEW HINGE WEB WAS INSTALLED IAW SRM 52-80-1, 51-10-2, 51-30-2, AND MM 51-20-11.
- [SDR CALA9801852](https://openairdocs.org/sdr/CALA9801852.md): Fitting · corroded · Sep 22, 1998 · N14788 · Boeing 727232 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING NR 6 FLAP TRACK FORWARD ATTACH FITTING CORRODED. THE FLAP TRACK FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA9801851](https://openairdocs.org/sdr/CALA9801851.md): Skin · lightning strike · Sep 22, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO STATIC PORT SKIN ON RT FUSELAGE FORWARD OF FORWARD PIT DOOR AT STA 500. THE DAMAGE WAS REPAIRED IAW SRM 53-30-03.
- [SDR CALA9801847](https://openairdocs.org/sdr/CALA9801847.md): Floorbeam · corroded · Sep 21, 1998 · N14788 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND UPPER SURFACE OF FLOORBEAM CORRODED AT BS 1166, RBL 50 TO RBL 66. THE CORROSION WAS REMOVED AND A REPAIR STRAP WAS INSTALLED IAW SRM 51-30-5, 51-10-2, 51-30-2, AND ECRA 5321-01029.
- [SDR CALA9801835](https://openairdocs.org/sdr/CALA9801835.md): Angle · corroded · Sep 21, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND NOSE RADOME AREA LOWER L-ANGLE CORRODED AT FS 178, LBL 6 TO RBL 6. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2 AND MM 51-20-0.
- [SDR CALA9801834](https://openairdocs.org/sdr/CALA9801834.md): Splice · corroded · Sep 20, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT FORWARD CARGO BUTT SPLICE NR 6 AND BUTT SPLICE AT BS 720 TO 730 CORRODED. NEW BUTT SPLICES WERE INSTALLED IAW SRM 51-20-1, FIGURE 7, 51-10-2, MM 51-20-11.
- [SDR CALA9801833](https://openairdocs.org/sdr/CALA9801833.md): Seat Track · corroded · Sep 20, 1998 · N14788 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND RT SEAT TRACK CORRODED AT STA 1132-113 TO, RBL 48. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-5, FIGURE 7, 51-30-5, 51-10-2, 53-10-4, AND MM 51-20-11.
- [SDR CALA9801832](https://openairdocs.org/sdr/CALA9801832.md): Angle · corroded · Sep 20, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ANGLE CORRODED BELOW FORWARD FLIGHT ATTENDANT'S SEAT AT STA 303.9 FROM LBL 12 TO LBL 50. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-40-3, 51-30-5, 53-10-2, AND MM 51-20-11.
- [SDR CALA9801830](https://openairdocs.org/sdr/CALA9801830.md): Rib · cracked · Sep 19, 1998 · N14788 · Boeing 727232 · Leading Edge Devices
  > INSPECTION FOUND A.5 INCH CRACK IN RT WING NR 5 SLAT INBOARD AND OUTBOARD RIBS AT ACTUATOR ROD END ATTACH POINT. BOTH THE INBOARD AND OUTBOARD RIBS WERE REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA9801829](https://openairdocs.org/sdr/CALA9801829.md): Floor · corroded · Sep 19, 1998 · N14788 · Boeing 727232 · Fuselage Floor Panel
  > INSPECTION FOUND COCKPIT LT SIDE FLOOR PANEL CORRODED. A NEW FLOOR PANEL WAS INSTALLED IAW SRM ECRA 5320-01448.
- [SDR CALA9801827](https://openairdocs.org/sdr/CALA9801827.md): Frame · cracked · Sep 19, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND C-3 CARGO DOOR CUTOUT FORWARD FRAME LOWER CORNER CRACKED OUT OF BOTTOM STOP FITTING UPPER INBOARD BOLT HOLE AND LOWER PART OF FRAME WAS CORRODED. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 51-40-3. THE CRACK WAS 1.
- [SDR CALA9801826](https://openairdocs.org/sdr/CALA9801826.md): Fitting · corroded · Sep 19, 1998 · N14788 · Boeing 727232 · Vertical Stabilizer
  > INSPECTION FOUND TOP OF VERTICAL STABILIZER LT HORIZONTAL HINGE ATTACH FITTINGS CORRODED. THE FITTINGS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-4, AND ECRA 5550-01033.
- [SDR CALA9801825](https://openairdocs.org/sdr/CALA9801825.md): Stringer · cracked · Sep 19, 1998 · N14788 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 4 INCH CRACK IN STRINGER 14L AT STA 900. THE CRACKED SECTION OF STRINGER WAS REPLACED IAW SRM 51-30-2.
- [SDR CALA9801824](https://openairdocs.org/sdr/CALA9801824.md): Web · corroded · Sep 19, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND RT AFT LAV FLOOR WEB CORRODED VANITY PLUMBING FITTING. THE FLOOR WEB WAS REMOVED, A NEW LAV FLOOR WEB, DOUBLER, AND FILLER WERE INSTALLED IAW SRM 51-40-2, 51-30-2, 51-10-2 AND MM 51-20-11.
- [SDR CALA9801823](https://openairdocs.org/sdr/CALA9801823.md): Press Panel · cracked · Sep 18, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.1875 INCH CRACK IN NLG RT SIDE PRESSURE PANEL OUT OF FASTENER HOLE AT BS 271, WL 185. THE EXISTING DOUBLER WAS REMOVED IAW SRM 51-30-2. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, PAGE 6A. A DOUBLER WAS INSTALLED IAW SRM 51-30-2, 51-10-2
- [SDR CALA9801822](https://openairdocs.org/sdr/CALA9801822.md): Floorbeam · corroded · Sep 18, 1998 · N14788 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 1130, RBL 26 TO RBL 34 AND LBL 62. THE FLOORBEAM AREAS WERE REPAIRED IAW ECRA 5321-01028 AND ECRA 5321-01027.
- [SDR CALA9801821](https://openairdocs.org/sdr/CALA9801821.md): Frame · corroded · Sep 18, 1998 · N14788 · Boeing 727232 · Fuselage Main, Frame
  > INSPECTION FOUND SIDE WALL SUPPORT FRAME CORRODED AT STA 720D ABOVE STRINGER 26R. THE CORRODED SECTION OF SUPPORT FRAME WAS REMOVED. A REPAIR ANGLE AND DOUBLER WERE INSTALLED IAW SRM 51-40-3, 51-10-2, 51-50-2 AND MM 51-20-11.
- [SDR CALA9801820](https://openairdocs.org/sdr/CALA9801820.md): Channel · cracked · Sep 18, 1998 · N14788 · Boeing 727232 · Cargo/Baggage Doors
  > INSPECTION FOUND C-1 CARGO DOOR UNDER LOWER LIGHT HAD A PIECE OF PAN CRACKED OUT. THE PAN CHANNEL WAS REMOVED, A REPAIR WAS INSTALLED IAW SRM 52-30-1, 51-10-2, 51-30-2 AND MM 51-20-12.
- [SDR CALA9801819](https://openairdocs.org/sdr/CALA9801819.md): Angle · cracked · Sep 18, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND 8 INCH CRACK IN L-ANGLE AT STA 1166, STRINGER 26L TO 26R. THE ANGLE WAS REMOVED, A REPAIR ANGLE, NUT PLATES, AND RADIUS BLOCK WERE INSTALLED IAW SRM 51-40-3, 51-10-2, 51-30-2 AND MM 51-20-11.
- [SDR CALA9801818](https://openairdocs.org/sdr/CALA9801818.md): Panel · cracked · Sep 18, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A.5 INCH CRACK IN PANEL NR 3338. THE CRACKED AREA WAS CUT OUT, A WEB AND DOUBLER REPAIR WAS INSTALLED IAW SRM 51-20-1, 51-30-2, 51-10-2 AND MM 51-20-11.
- [SDR CALA9801817](https://openairdocs.org/sdr/CALA9801817.md): Chord · corroded · Sep 18, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LT UPPER CHORD CORRODED INSIDE NOSE WHEEL WELL AT STA 292, LBL 20. THE CHORD WAS REMOVED AND A NEW CHORD WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9801811](https://openairdocs.org/sdr/CALA9801811.md): Stiffener · corroded · Sep 17, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND VERTICAL STIFFENER CORRODED AT RT FUSELAGE STA 340. A NEW STIFFENER WAS INSTALLED IAW ECRA 5300-01196 AND SRM 51-30-2.
- [SDR CALA9801810](https://openairdocs.org/sdr/CALA9801810.md): Stringer · corroded · Sep 17, 1998 · N14788 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 25R CORRODED AT STA 1140 TO 1183. THE STRINGER WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-10-3.
- [SDR CALA9801798](https://openairdocs.org/sdr/CALA9801798.md): Angle · corroded · Sep 16, 1998 · N14788 · Boeing 727232 · Wing Miscellaneous Structure
  > INSPECTION FOUND LT WING NR 3 SPOILER L-ANGLE CORRODED AT INBOARD SIDE OF TRANSMISSION, WS 491. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-10-2 AND 51-10-3.
- [SDR CALA9801797](https://openairdocs.org/sdr/CALA9801797.md): Mechanism · out of adjust · Sep 16, 1998 · N14788 · Boeing 727232 · Emergency Exits
  > THE LT FORWARD OVERWING EMERGENCY EXIT DOOR FAILED PULL CHECK. THE PULL FORCE ON THE DOOR WAS ADJUSTED TO SPECIFICATION IAW MM 52-21-0.
- [SDR CALA9801796](https://openairdocs.org/sdr/CALA9801796.md): Skin · corroded · Sep 16, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND CORROSION IN FUSELAGE SKIN UNDER RIVET HEAD AT BS 560 TO 580, STRINGER 5R. THE CORRODED AREA OF SKIN WAS CUT OUT AND A DOUBLER STRAP REPAIR WAS INSTALLED IAW SRM 53-30-8, 51-10-6, 51-20-4, AND 51-30-2.
- [SDR CALA9801777](https://openairdocs.org/sdr/CALA9801777.md): Chord · corroded · Sep 15, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND SHEAR TIE T-CHORD CORRODED AT STA 351.5, BL 0, WL 148.5. THE T-CHORD WAS REMOVED AND A NEW T-CHORD WAS INSTALLED IAW SRM 51-10-02.
- [SDR CALA9801776](https://openairdocs.org/sdr/CALA9801776.md): Stringer · corroded · Sep 15, 1998 · N14788 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 23R CORRODED AT LOWER NOSE WHEEL WELL RT LAP SEAM STA 294.5. A STRINGER REPAIR WAS INSTALLED IAW SRM 53-10-3, FIGURE 1.
- [SDR CALA9801775](https://openairdocs.org/sdr/CALA9801775.md): Skin · impacted · Sep 15, 1998 · N14788 · Boeing 727232 · Cargo/Baggage Doors
  > INSPECTION FOUND LIGHTNING STRIKE DAMAGE TO C-1 DOOR SKIN. DOUBLER WAS INSTALLED IAW SRM 52-00-3, FIGURE 4 AND ECRA 5232-01004.
- [SDR CALA9801774](https://openairdocs.org/sdr/CALA9801774.md): Skin · damaged · Sep 15, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LIGHTNING STRIKE DAMAGE ON FUSELAGE SKIN AT STA 448 TO 451, STRINGER 25R, AND AT STA 380, STRINGER 23R. DOUBLERS WERE INSTALLED IAW SRM 53-30-3.
- [SDR CALA9801773](https://openairdocs.org/sdr/CALA9801773.md): Seat Track · corroded · Sep 15, 1998 · N14788 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND LT SEAT TRACK CORRODED AT STA 1136, LBL 46. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-10-2, 51-10-2, 51-30-2, AND MM 51-20-12.
- [SDR CALA9801772](https://openairdocs.org/sdr/CALA9801772.md): Channel · cracked · Sep 15, 1998 · N14788 · Boeing 727232 · Nacelle/Pylon Structure
  > INSPECTION FOUND A 1.75 INCH CRACK IN NR 3 ENGINE PYLON UPPER FIXED COWL FORWARD END U-CHANNEL. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-3.
- [SDR CALA9801771](https://openairdocs.org/sdr/CALA9801771.md): Strap · corroded · Sep 15, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO PIT LT LOWER SIDE WALL PANEL STRAP CORRODED AT STA 1050. A NEW STRAP WAS INSTALLED IAW SRM 51-10-6.
- [SDR CALA9801770](https://openairdocs.org/sdr/CALA9801770.md): Floorbeam · corroded · Sep 15, 1998 · N14788 · Boeing 727232 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT STA 344, RBL 65 TO LBL 65. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 51-30-2, 53-10-2, 53-10-8, FIGURE 9, AND MM 51-20-12.
- [SDR CALA9801756](https://openairdocs.org/sdr/CALA9801756.md): Panel · corroded · Sep 14, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND LT TRANSITION PANEL CORRODED IN FORWARD CARGO PIT AT FS 660 TO 720D. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-12.
- [SDR CALA9801755](https://openairdocs.org/sdr/CALA9801755.md): Panel · corroded · Sep 14, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FLOOR TRANSITION PANEL CORRODED AT BS 720A-720D, STRINGER 26R. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-12.
- [SDR CALA9801754](https://openairdocs.org/sdr/CALA9801754.md): Panel · corroded · Sep 14, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND RT TRANSITION PANEL CORRODED AROUND NUT PLATES IN FORWARD CARGO COMPARTMENT AT STA 620-720D. THE PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-10-2, 51-30-2, AND MM 51-20-12.
- [SDR CALA9801753](https://openairdocs.org/sdr/CALA9801753.md): Floor Pan · corroded · Sep 14, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND CABIN INTERIOR CENTER AISLE FLOOR PAN CORRODED AT BS 1173, RBL 22. THE FLOOR PAN WAS REMOVED AND A NEW FLOOR PAN WAS INSTALLED IAW SRM 51-30-2, 51-10-6, MM 51-20-11.
- [SDR CALA9801730](https://openairdocs.org/sdr/CALA9801730.md): Intercostal · corroded · Sep 13, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND INTERCOSTAL CORRODED AT FS 303.9, LBL 0 TO 12. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9801729](https://openairdocs.org/sdr/CALA9801729.md): Panel · corroded · Sep 13, 1998 · N14788 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND FORWARD CARGO PIT LT TRANSITION PANEL CORRODED FROM STA 530-550. THE PANEL WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-10-2, AND MM 51-20-12.
- [SDR CALA9801728](https://openairdocs.org/sdr/CALA9801728.md): Bracket · cracked · Sep 13, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 2 INCH AND 1.5 INCH CRACK IN CABIN FLOOR SUPPORT BRACKET AT STA 303.9, LBL 12. THE FLOOR SUPPORT BRACKET WAS REMOVED AND NEW BRACKET WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9801727](https://openairdocs.org/sdr/CALA9801727.md): Frame · corroded · Sep 13, 1998 · N14788 · Boeing 727232 · Fuselage Main, Frame
  > INSPECTION FOUND CORROSION AT HOLE OF LT UPPER DOOR FRAME STA 1183, WL 273, LBL 19.22. REPAIRED IAW ECRA 5310-03765.
- [SDR CALA9801726](https://openairdocs.org/sdr/CALA9801726.md): Subfloor · corroded · Sep 13, 1998 · N14788 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FORWARD LAV SUBFLOOR CORRODED AT STA 340, RBL 42-60. THE LAV SUBFLOOR WAS REMOVED AND REPLACED IAW SRM 51-20-1.

Next page: https://openairdocs.org/deregistered/N14788-2000-08-29/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 = 'N14788' AND deregistration_id = 'N14788-2000-08-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N14788-2000-08-29/reports

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