# Service difficulty reports: N15790, cancelled Nov 27, 2012

A list on [N15790, cancelled Nov 27, 2012](https://openairdocs.org/deregistered/N15790-2012-11-27.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 · 75 reports

- [SDR MZZA00013](https://openairdocs.org/sdr/MZZA00013.md): Skin · corroded · Jun 7, 2000 · N15790 · Boeing 727232 · Fuselage Main, Plate/Skin
  > GUM - LOWER FUSELAGE APPROXIMATELY 6 O''CLOCK POSITION HAS CORROSION BUILD UP THROUGH OUT LEFT AND RIGHT FORWARD OF RAM AIR INLET. SKIN OF AIRCRAFT CORRODED AT BS 720A - 720B BETWEEN S28L AND S27R. AREA OF DEFECT DIRECTLY ABOVE RAM AIR DOOR INLET SCOOP. MAI
- [SDR MZZA00007](https://openairdocs.org/sdr/MZZA00007.md): Toggle · cracked · Apr 7, 2000 · N15790 · Boeing 727232 · Trailing Edge Flap Control System
  > FLT 977 - AFTER TAKEOFF, INDICATION OF LEADING EDGE FLAPS AND SLATS EXTENDED INDICATED AT CONTROL PANEL AND GREEN LIGHT MAIN FLAPS OUTBOARD INDICATION STOPPED AT 4 DEGREES, INBOARD INDICATION STOPPED AT 2 DEGREES, AILERON L-1 DEGREE, RUDDER L-2.5 DEGREES TO GE
- [SDR MZZA99127](https://openairdocs.org/sdr/MZZA99127.md): Stringer · corroded · Jun 30, 1999 · N15790 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 5 SQUARE INCH AREA CORROSION WAS FOUND ON STRINGER 27L BETWEEN BS 720F PLUS 6 AND BS 740. THE CORRODED PART OF STRINGER WAS TRIMMED OUT AND REPAIRED PER B727 CHAP 53-10-03 FIG 1. (M)
- [SDR MZZA99135](https://openairdocs.org/sdr/MZZA99135.md): Skin · corroded · Jun 24, 1999 · N15790 · Boeing 727232 · Fuselage Main, Plate/Skin
  > TNN - DURING D-CHECK INSPECTION ON AIR ASIA, A 4 INCH BY 32 INCH AREA CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN BS 448 AND BS 480, STRINGER 26R. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-30-03 FIG 3. (M)
- [SDR MZZA99123](https://openairdocs.org/sdr/MZZA99123.md): Channel · cracked · Jun 20, 1999 · N15790 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1. 5 INCH LONG CRACK WAS FOUND ON U-CHANNEL ATTACHED TO RIGHT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1273. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 CHAPTER 51-40-03 AND 51-30-02. (M)
- [SDR MZZA99125](https://openairdocs.org/sdr/MZZA99125.md): Splice · corroded · Jun 18, 1999 · N15790 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH IG CORROSION WAS FOUND ON STRINGER 30 SPLICE ON CARGO COMPARTMENT AT BS 1010. THE DAMAGED PART WAS REMOVED AND REPLACED WITH NEW ONE PER B727 CHAPTER 53-10-03 FIG 1. (M)
- [SDR MZZA99118](https://openairdocs.org/sdr/MZZA99118.md): Stringer · cracked · Jun 18, 1999 · N15790 · Boeing 727232 · Wing, Longeron/Stringer
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUND CRACK ON RIGHT WING UPPER VENT STRINGER 12 AND WS 686.5 WEB ATTACHMENT. THE CRACKED STRINGER WAS TRIMMED OUT AND REPAIRED PER EA 5762-01050 PART 3. (M)
- [SDR MZZA99117](https://openairdocs.org/sdr/MZZA99117.md): Stringer · cracked · Jun 18, 1999 · N15790 · Boeing 727232 · Wing, Longeron/Stringer
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUND CRACK ON RIGHT WING UPPER VENT STRINGER 11 AND WS 629 WEB ATTACHMENT. THE CRACKED STIFFENER WAS TRIMMED OUT AND REPAIRED PER EA 5762-01050 PART 3. (M)
- [SDR MZZA99126](https://openairdocs.org/sdr/MZZA99126.md): Stringer · corroded · Jun 16, 1999 · N15790 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH BY 32 INCH AREA CORROSION WAS FOUND ON STRINGER 26R BETWEEN BS 448 AND BS 480. THE CORRODED PART OF STRINGER WAS TRIMMED AND REPAIRED PER B727 CHAPTER 53-10-03 FIG 1. (M)
- [SDR MZZA99112](https://openairdocs.org/sdr/MZZA99112.md): Web · cracked · Jun 16, 1999 · N15790 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.625 INCH LONG CRACK WAS FOUND ON LEFT LOWER TORQUE BOX VERTICAL WEB AT BS 1213. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 51-40-02 FIG 1. (M)
- [SDR MZZA99120](https://openairdocs.org/sdr/MZZA99120.md): Frame · corroded · Jun 15, 1999 · N15790 · Boeing 727232 · Fuselage Main, Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 30 SQUARE INCH AREA IG CORROSION WAS FOUND ON FUSELAGE FRAME AT BS 219 AND RT WL 233. THE CORRODED FRAME WAS TRIMMED OUT AND REPAIRED PER SRM 51-40-03. (M)
- [SDR MZZA99140](https://openairdocs.org/sdr/MZZA99140.md): Seat Track · corroded · Jun 11, 1999 · N15790 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH BY 4 INCH AREA IG CORROSION WAS FOUND ON PASSENGER FLOOR SEAT TRACK AT BS 395 AND RBL 40. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-10-05 FIG 1. (M)
- [SDR MZZA99134](https://openairdocs.org/sdr/MZZA99134.md): Floorbeam · corroded · Jun 10, 1999 · N15790 · Boeing 727232 · Fuselage Main, Floor Beam
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY 6 INCH AREA IG CORROSION WAS FOUND ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT BS 328 FROM LBL 01 TO RBL 05. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 51-40-04 FIG 2
- [SDR MZZA99133](https://openairdocs.org/sdr/MZZA99133.md): Seat Track · corroded · Jun 10, 1999 · N15790 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR SEAT TRACK BETWEEN BS 360/380 ALONG RBL 18. THE DAMGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-10-05 FIG 1. (M)
- [SDR MZZA99132](https://openairdocs.org/sdr/MZZA99132.md): Seat Track · corroded · Jun 10, 1999 · N15790 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > TNN - DURING D-CHECK INSPECTON ON AIRCRAFT AT AIR ASIA, A 1 INCH BY 20 INCH AREA IG CORROSION WAS FOUND ON PASSENGER CABIN FLOOR SEAT TRACK BETWEEN BS 360 AND 380 ALONG RBL 22 AND RBL 24. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-1
- [SDR MZZA99119](https://openairdocs.org/sdr/MZZA99119.md): Stiffener · corroded · Jun 8, 1999 · N15790 · Boeing 727232 · Wing Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON RIGHT WING FRONT SPAR STIFFENER AT SS 58. THE CORRODED WAS REMOVED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M)
- [SDR MZZA99142](https://openairdocs.org/sdr/MZZA99142.md): Frame · cracked · Jun 5, 1999 · N15790 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.5 INCH LONG CRACK WAS FOUND ON C3 DOOR FORWARD FLANGE AT STRINGER 27R ON CARGO COMPARTMENT. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW ONE PER B727 CHAP 53-10-04 FIG 1. (M)
- [SDR MZZA99141](https://openairdocs.org/sdr/MZZA99141.md): Floorbeam · corroded · Jun 5, 1999 · N15790 · Boeing 727232 · Fuselage Main, Floor Beam
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH AREA IG CORROSION WAS FOUND ON BS 1148 FLOORBEAM UPPER CHORD AT LBL 10. THE CORROED PART OF UPPER WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAP 53-10-08 FIG 3. (M)
- [SDR MZZA99128](https://openairdocs.org/sdr/MZZA99128.md): Frame · corroded · Jun 5, 1999 · N15790 · Boeing 727232 · Fuselage Main, Frame
  > DURNIG D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 SQUARE INCH IG CORROSION WAS FOUND ON BS 1148 FRAME FORWARD FLANGE ON CARGO COMPARTMENT. THE CORRODED PART OF FRAME WAS TRIMMED OUT AND REPAIRED PER B727 CHAP 53-10-04 FIG 1. (M)
- [SDR MZZA99122](https://openairdocs.org/sdr/MZZA99122.md): Spar Chord · corrosion · Jun 5, 1999 · N15790 · Boeing 727232 · Vertical Stabilizer, Spar/Rib
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON VERTICAL STABILIZER FRONT SPAR LEFT CHORD AT FS 54. THE CORRODED AREA IS TRIMMED OUT AND REPAIRED PER ECRA 5530-01250. ISSUE A NEW DIP NR CM 556 TO READ AS FOLLOWS WITHIN 11 MONT
- [SDR MZZA99137](https://openairdocs.org/sdr/MZZA99137.md): Skin · corroded · Jun 4, 1999 · N15790 · Boeing 727232 · Fuselage Main, Plate/Skin
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 SQUARE INCH IG CORROSION WAS FOUND ON FUSELAGE SKIN BETWEEN STRINGER 27R AND BS 720D PLUS 13. THE CORRODED SKIN WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-30-03 FIG 3. (M)
- [SDR MZZA99129](https://openairdocs.org/sdr/MZZA99129.md): Shear Tie · corroded · Jun 4, 1999 · N15790 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 SQUARE INCH AREA IG CORROSION WAS FOUND ON BS 950E SHEAR TIE ON CARGO COMPARTMENT. THE CORRODED SHEAR TIE WAS REMOVED AND REPLACED WITH NEW ONE PER B727 CHAP 53-10-04 FIG 14. (M)
- [SDR MZZA99124](https://openairdocs.org/sdr/MZZA99124.md): Skin · corroded · Jun 4, 1999 · N15790 · Boeing 727232 · Fuselage Main, Plate/Skin
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 5 SQUARE INCH IG CORROSION WAS FOUND ON FUSELAGE SKIN AT BS 720F PLUS 4 AND STRINGER 28L - STRINGER 26R. THE CORRODED AREA WAS CLEANED UP AND REPAIRED PER EC/RA 5330-02842. (M)
- [SDR MZZA99136](https://openairdocs.org/sdr/MZZA99136.md): Skin · cracked · Jun 3, 1999 · N15790 · Boeing 727232 · Fuselage Main, Plate/Skin
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A.75 INCH LONG CRACK WAS FOUND ON FUSELAGE SKIN BETWEEN STRINGER 28R AND BS 720A PLUS 4. THE CORRODED SKIN WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 53-30-03 FIG 3. (M)
- [SDR MZZA99138](https://openairdocs.org/sdr/MZZA99138.md): Beam · corroded · Jun 2, 1999 · N15790 · Boeing 727232 · Horizontal Stabilizer Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG IG CORROSION WAS FOUND ON RIGHT STABILIZER UPPER T/E BEAM AT ELEVATOR STATION 190. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-05 FIG 1. (M)
- [SDR MZZA99139](https://openairdocs.org/sdr/MZZA99139.md): Beam · corrosion · Jun 1, 1999 · N15790 · Boeing 727232 · Horizontal Stabilizer Structure
  > TNN - DURING D-CHECK INSPECTION AT AIR ASIA, A 3 INCH LONG CORROSION WAS FOUND ON LEFT STAB UPPER T/E BEAM AT ELEV STATION 119. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-06 FIG 1. (M)
- [SDR MZZA99131](https://openairdocs.org/sdr/MZZA99131.md): Seat Track · corroded · Jun 1, 1999 · N15790 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON BS 1130 AND LBL 46 SEAT TRACK. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-05 FIG 1. (M)
- [SDR MZZA99130](https://openairdocs.org/sdr/MZZA99130.md): Beam · corrosion · Jun 1, 1999 · N15790 · Boeing 727232 · Horizontal Stabilizer Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG IG CORROSION WAS FOUND ON LEFT STABILIZER UPPER T/E BEAM AT ELEVATOR STATION 155. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-10-05 FIG 1. (M)
- [SDR MZZA99121](https://openairdocs.org/sdr/MZZA99121.md): Skin · cracked · Jun 1, 1999 · N15790 · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A RIGHT VERTICAL STABILIZER SKIN WAS FOUND CRACKED JUST AFT TO THE BS 1183 BULKHEAD AT APPROX WL 302. NO ADDITIONAL REWORK OF THE CRACK IS NECESSARY DUE TO WITHIN LIMIT. ISSUE A DIP NR CM558 TO INSPECT
- [SDR MZZA99116](https://openairdocs.org/sdr/MZZA99116.md): Web · crack · May 31, 1999 · N15790 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH LONG CRACK WAS FOUND ON LEFT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1275. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 51-40-02 FIG 1. (M)
- [SDR MZZA99115](https://openairdocs.org/sdr/MZZA99115.md): Channel · cracked · May 31, 1999 · N15790 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.25 INCH LONG CRACK WAS FOUND ON U-CHANNEL WHICH IS ATTACHED LEFT LOWER TORQUE BOX HORIZONTAL WEB AT BS 1273. THE DAMAGED ANGLES WERE REMOVED AND REPLACED PER B727 SRM CHAP 51-40-03. (M)
- [SDR MZZA99114](https://openairdocs.org/sdr/MZZA99114.md): Web · cracked · May 31, 1999 · N15790 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO PLACES 1. 5 INCH AND.625 INCH LONG CRACKS WERE FOUND ON L-ANGLES WHICH ARE ATTACHED TO RGHT LOWER TORQUE BOX VERTICAL WEB AT BS 1263. THE DAMAGED ANGLES WERE REMOVED AND REPLACED PER B727 SRM CHAPT
- [SDR MZZA99113](https://openairdocs.org/sdr/MZZA99113.md): Web · cracked · May 31, 1999 · N15790 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1 INCH LONG CRACK WAS FOUND ON LEFT LOWER TORQUE BOX VERTICAL WEB AT BS 1229. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 51-40-02 FIG 1. (M)
- [SDR CALA9802145](https://openairdocs.org/sdr/CALA9802145.md): Fuse · failed · Dec 7, 1998 · N15790 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND AFT SECTION OF AISLE EMERGENCY PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND PINS PULLED OUT OF CONNECTOR AT ROW 20 SEAT LIGHT PIGTAIL. THE CONNECTOR WAS REPINNED. ALSO, FOUND AFT POWER SUPPLY BASE F-2 FUSE BLOWN. THE FUSE WAS REMOVED AND RE
- [SDR CALA9801846](https://openairdocs.org/sdr/CALA9801846.md): Wire · broken · Sep 21, 1998 · N15790 · Boeing 727232 · Light System Wiring
  > INSPECTION FOUND R-1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. MAINTENANCE FOUND AND REPAIRED A BROKEN WIRE AT LIGHT ASSEMBLY.
- [SDR CALA9801845](https://openairdocs.org/sdr/CALA9801845.md): Skin · corroded · Sep 21, 1998 · N15790 · Boeing 727232 · Trailing Edge Flaps
  > INSPECTION FOUND THE RT WING INBOARD MIDFLAP CORRODED AROUND TWO RIVETS ON UPPER SURFACE. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-1.
- [SDR CALA9801844](https://openairdocs.org/sdr/CALA9801844.md): Skin · corroded · Sep 21, 1998 · N15790 · Boeing 727232 · Spoilers
  > INSPECTION FOUND NR 5 SPOILER CORRODED ALONG TOP EDGES. THE NR 5 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.
- [SDR CALA9801843](https://openairdocs.org/sdr/CALA9801843.md): Skin · delaminated · Sep 21, 1998 · N15790 · Boeing 727232 · Spoilers
  > INSPECTION FOUND THE NR 2 SPOILER DELAMINATED AFT OF INBOARD HINGE. THE NR 2 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.
- [SDR CALA9801842](https://openairdocs.org/sdr/CALA9801842.md): Skin · delaminated · Sep 21, 1998 · N15790 · Boeing 727232 · Trailing Edge Flaps
  > INSPECTION FOUND RT WING INBOARD TRAILING EDGE AFT FLAP DELAMINATED AT OUTBOARD AND INBOARD TRAILING EDGE CORNER. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-51-1.
- [SDR CALA9801841](https://openairdocs.org/sdr/CALA9801841.md): Skin · delaminated · Sep 21, 1998 · N15790 · Boeing 727232 · Spoilers
  > INSPECTION FOUND NR 7 SPOILER DELAMINATED AT LOWER OUTBOARD AFT TRAILING EDGE. THE NR 7 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.
- [SDR CALA9801840](https://openairdocs.org/sdr/CALA9801840.md): Skin · delaminated · Sep 21, 1998 · N15790 · Boeing 727232 · Trailing Edge Flaps
  > INSPECTION FOUND LT OUTBOARD AFT FLAP OUTBOARD LOWER CORNER DELAMINATED. THE FLAP WAS REMOVED AND REPLACED IAW MM 27-61-12.
- [SDR CALA9801839](https://openairdocs.org/sdr/CALA9801839.md): Skin · corroded · Sep 21, 1998 · N15790 · Boeing 727232 · Spoilers
  > INSPECTION FOUND NR 1 SPOILER CORRODED ALONG OUTBOARD EDGE AND DELAMINATED ON TOP. THE NR 1 SPOILER WAS REMOVED AND REPLACED IAW MM 27-61-1.
- [SDR CALA9801816](https://openairdocs.org/sdr/CALA9801816.md): Stiffener · cracked · Sep 18, 1998 · N15790 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN NOSE WHEEL WELL STIFFENER AT STA 234, LBL 20. THE STIFFENER WAS REPAIRED IAW SRM 51-10-2.
- [SDR CALA9801815](https://openairdocs.org/sdr/CALA9801815.md): Chord · cracked · Sep 18, 1998 · N15790 · Boeing 727232 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN LT WING LOWER CHORD AT NR 7 SPOILER ACTUATOR. THE CRACKED AREA WAS CUT OUT, STRAPS AND CHORD ANGLE WERE INSTALLED IAW ECRA 5720-01680 AND SRM 51-10-2.
- [SDR CALA9801814](https://openairdocs.org/sdr/CALA9801814.md): Stiffener · corroded · Sep 18, 1998 · N15790 · Boeing 727232 · Wing Miscellaneous Structure
  > INSPECTION FOUND LT WING FRONT SPAR STIFFENER CORRODED ON INBOARD SIDE CENTER AT STA 224. THE STIFFENER WAS REMOVED AND A NEW STIFFENER WAS INSTALLED IAW SRM 51-30-2 AND 51-20-4.
- [SDR CALA9801790](https://openairdocs.org/sdr/CALA9801790.md): Seat Track · corroded · Sep 16, 1998 · N15790 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION FOUND SEAT TRACK CORRODED AT FS 1090 TO 1130, RBL 45. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-10-1 AND 51-10-2.
- [SDR CALA9801789](https://openairdocs.org/sdr/CALA9801789.md): Skin · delaminated · Sep 16, 1998 · N15790 · Boeing 727232 · Aileron Tabs
  > INSPECTION FOUND LT INBOARD AILERON TAB TRAILING EDGE SEPARATED IN TWO AREAS. THE AILERON TAB WAS REMOVED AND REPLACED IAW MM 27-10-11.
- [SDR CALA9801788](https://openairdocs.org/sdr/CALA9801788.md): Bracket · corroded · Sep 16, 1998 · N15790 · Boeing 727232 · Spoilers
  > INSPECTION FOUND NR 7 SPOILER ATTACH SUPPORT BRACKET CORRODED. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2.
- [SDR CALA9801787](https://openairdocs.org/sdr/CALA9801787.md): Beam · cracked · Sep 16, 1998 · N15790 · Boeing 727232 · Wing Miscellaneous Structure
  > INSPECTION FOUND A.375 INCH CRACK IN LT WING TRAILING EDGE J-BEAM ABOVE NR 7 SPOILER ACTUATOR. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW ECRA 5750-02914 AND SRM 51-10-6.
- [SDR CALA9801786](https://openairdocs.org/sdr/CALA9801786.md): Battery · discharged · Sep 16, 1998 · N15790 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND MAIN CABIN EMERGENCY LIGHT AT ROW 8 HAD A WEAK BATTERY. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW MM 33-50-00.

Next page: https://openairdocs.org/deregistered/N15790-2012-11-27/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 = 'N15790' AND deregistration_id = 'N15790-2012-11-27'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N15790-2012-11-27/reports

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