# Service difficulty reports: N15781, cancelled Feb 28, 2018

A list on [N15781, cancelled Feb 28, 2018](https://openairdocs.org/deregistered/N15781-2018-02-28.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 3 · 101 reports

- [SDR MZZA00002](https://openairdocs.org/sdr/MZZA00002.md): Battery · inoperative · Jan 24, 2000 · N15781 · Boeing 727232 · Emergency Lighting
  > GUM - FOUND 2L SERVICE DOOR EMERGNECY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK PER MM 33-50-01. OPS CHECK GOOD AND RELEASED AIRCRAFT FOR SERVICE. (M)
- [SDR MZZA99239](https://openairdocs.org/sdr/MZZA99239.md): Housing · cracked · Dec 24, 1999 · N15781 · Boeing 727232 · Landing Gear Retraction/Extension System
  > GUM - FLT 988 - EN ROUTE TO SPN, STARTED NOTICING A LOSS OF A-SYSTEM HYDRAULIC QUANTITY. REMOVED AND REPLACED MLG SEQUENCE VALVE PER MM 32-32-31. (X)
- [SDR MZZA99199](https://openairdocs.org/sdr/MZZA99199.md): T-Chord · corroded · Oct 26, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 SQUARE INCH IG CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER TEE OF STRINGER 29L. THE CORRODED T-CHORD SECTION WAS TRIMMED AND REPAIRED PER CMI EC/RA NR 5310-0397. (M)
- [SDR MZZA99226](https://openairdocs.org/sdr/MZZA99226.md): Control Cable · frayed · Oct 17, 1999 · N15781 · Boeing 727232 · Power Lever
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT ASIA, NR 3 ENGINE CONTROL CABLE (T3B) WAS FOUND FRAYED AT BS 1070. THE FRAYED CABLE WAS REMOVED AND REPLACED PER B727 MM CHAPTER 76-12-01 AND OPERATIONAL CHECK FOUND NORMAL. (M)
- [SDR MZZA99223](https://openairdocs.org/sdr/MZZA99223.md): Frame · corroded · Oct 12, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY 5 INCH AREA IG CORROSION WAS FOUND ON NLG BAY FUSELAGE FRAME AT BS 303 BETWEEN STRINGER 25L AND STRINGER 26L. THE CORRODED FRAME WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 53-30-03. (M)
- [SDR MZZA99190](https://openairdocs.org/sdr/MZZA99190.md): Fitting · corroded · Oct 11, 1999 · N15781 · Boeing 727232 · Auxiliary Gear (Tail Skid)
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON TAIL SKID DRAG LEFT HINGE FITTING IN TAIL SKID BAY. THE CORRODED FITTING WAS REMOVED AND REPLACED WITH A NEW ONE (P/N 65-25614-11) PER B727 SRM CHAPTER 51-10-01 AND 51-30-02.
- [SDR MZZA99224](https://openairdocs.org/sdr/MZZA99224.md): Tee · corroded · Oct 8, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON NOSE WHEEL WELL TEE CHORD BETWEEN BS 294-312 AT STRINGER 26L. THE CORRODED T-CHORD WAS TRIMMED AND REPAIRED PER CMI EC/RA NR 5310-03937. (M)
- [SDR MZZA99206](https://openairdocs.org/sdr/MZZA99206.md): Floorbeam · cracked · Oct 6, 1999 · N15781 · Boeing 727232 · Fuselage Main, Floor Beam
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG CRACK WAS FOUND ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT BS 740 AND LBL 25. THE CORRODED SECTION WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M)
- [SDR MZZA99203](https://openairdocs.org/sdr/MZZA99203.md): Floorbeam · cracked · Oct 6, 1999 · N15781 · Boeing 727232 · Fuselage Main, Floor Beam
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH LONG CRACK WAS FOUND ON PASSENGER CABIN FLOORBEAM UPPER CHORD AT BS 740. THE CORRODED SECTION WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 53-30-02 AND 51-10-01. (M)
- [SDR MZZA99195](https://openairdocs.org/sdr/MZZA99195.md): Stiffener · cracked · Oct 6, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.125 INCH LONG CRACK WAS FOUND ON BS 1183 BULKHEAD WEB FORWARD SIDE REINFORCEMENT BEAM INBOARD FLANGE AT LBL 36 AND WL 250. THE CORRODED SECTION WAS REPAIRED PER CMI EC/RA NR 5310-03930 USING KIT NR
- [SDR MZZA99194](https://openairdocs.org/sdr/MZZA99194.md): Stiffener · cracked · Oct 6, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A.625 INCH LONG CRACK WAS FOUND ON BS 1183 BULKHEAD WEB FORWARD SIDE REINFORCEMENT BEAM OUTBOARD FLANGE AT LBL 37 AND WL 250. THE DAMAGED SECTION WAS REPAIRED PER CMI EC/RA NR 5310-03930 USING KIT NR 6
- [SDR MZZA99220](https://openairdocs.org/sdr/MZZA99220.md): Frame · cracked · Oct 5, 1999 · N15781 · Boeing 727232 · Fuselage Main, Frame
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO 2 INCH AND 1.5 INCH LONG CRACKS WERE FOUND ON BS 1183 BULKHEAD FRAME INBOARD AND OUTBOARD FLANGE AT RBL 36 AND WL 238. THE DAMAGED SECTION WAS REPAIRED PER CMI EC/RA NR 5310-03930 USING KIT NR 65C34
- [SDR MZZA99208](https://openairdocs.org/sdr/MZZA99208.md): Bracket · corroded · Oct 5, 1999 · N15781 · Boeing 727232 · Passenger/Crew Doors
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, AN IG CORROSION WAS FOUND ON L2 CABIN DOOR FORWARD STOP FITTING SUPPORT BRACKET. THE CORRODED FITTING WAS REMOVED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M)
- [SDR MZZA99207](https://openairdocs.org/sdr/MZZA99207.md): Web · corroded · Oct 5, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON TAIL SKID DRAG FORWARD WEB AT BS 1184. THE CORRODED WEB WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 51-40-03. (M)
- [SDR MZZA99228](https://openairdocs.org/sdr/MZZA99228.md): Stiffener · corroded · Oct 4, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON LEFT KEEL BEAM STIFFENER LOWER END AT WS 930. THE CORRODED STIFFENER SECTION WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M)
- [SDR MZZA99227](https://openairdocs.org/sdr/MZZA99227.md): Stiffener · corroded · Oct 4, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION WAS FOUND ON LEFT KEEL BEAM STIFFENER LOWER END AT BS 920. THE CORRODED STIFFENER SECTION WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 51-40-04. (M)
- [SDR MZZA99204](https://openairdocs.org/sdr/MZZA99204.md): Frame · cracked · Sep 29, 1999 · N15781 · Boeing 727232 · Fuselage Main, Frame
  > TNN - DURING S-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG CRACK WAS FOUND ON FUSELAGE FRAME BETWEEN STRINGER 16R AND 17R AT BS 783.9. THE DAMAGED SECTION WAS TRIMMED AND REPAIRED PER BOEING DRAWING NR 65C36280 USING REPAIR KIT NR 65C36280-24. (M
- [SDR MZZA99191](https://openairdocs.org/sdr/MZZA99191.md): Skin · damaged · Sep 29, 1999 · N15781 · Boeing 727232 · Passenger/Crew Doors
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.5 INCH BY 1 INCH AREA DAMAGE WAS FOUND ON L2 CABIN DOOR SKIN FORWARD LOWER CORNER. THE DAMAGED AREA WAS TRIMMED AND REPAIRED PER B727 SRM CHAP 52-40-02. (M)
- [SDR MZZA99222](https://openairdocs.org/sdr/MZZA99222.md): Web · cracked · Sep 28, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, TWO CRACKS WERE FOUND ON LEFT LOWER TORQUE BOX VERTICAL WEB LIGHTENING HOLES AT BS 1223. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 51-40-02. (M)
- [SDR MZZA99221](https://openairdocs.org/sdr/MZZA99221.md): Gusset · corroded · Sep 28, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, IG CORROSION WAS FOUND ON GUSSET ATTACHED TO BS 950 LOWER TEE CHORD AND STRINGER 29L IN FLANGE. THE CORRODED GUSSET WAS REMOVED AND REPAIRED PER B727 SRM CHAPTER 51-10-01 AND 51-30-02. (M)
- [SDR MZZA99219](https://openairdocs.org/sdr/MZZA99219.md): Fitting · cracked · Sep 28, 1999 · N15781 · Boeing 727232 · Wing Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CRACK WAS FOUND ON LEFT WING BOTTLE PIN. THE CORRODED FITTING WAS REMOVED AND REPLACED WITH A NEW ONE POWER SRM 53-30-02. (M)
- [SDR MZZA99218](https://openairdocs.org/sdr/MZZA99218.md): Gusset · corroded · Sep 28, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, AN IG CORROSION WAS FOUND ON GUSSET ATTACHED TO BS 950 BULKHEAD LOWER TEE CHORD AND STRINGER 29R INBOARD FLANGE. THE CORRODED GUSSET WAS REMOVED AND REPLACED WITH A NEW ONE PER B727 SRM CHAPTER 51-10-01
- [SDR MZZA99216](https://openairdocs.org/sdr/MZZA99216.md): Stringer · cracked · Sep 28, 1999 · N15781 · Boeing 727232 · Wing, Longeron/Stringer
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON RIGHT WING UPPER STRINGER S-13 ATTACHED TO WS 629 RIB. THE CRACK WAS STOP DRILLED AND REPAIRED PER CMI EA NR 5762-01050. (M)
- [SDR MZZA99215](https://openairdocs.org/sdr/MZZA99215.md): Rib · cracked · Sep 28, 1999 · N15781 · Boeing 727232 · Wing, Rib/Bulkhead
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON RIGHT WING INSPAR WS 738.5 RIB UPPER FLANGE ATTACHED TO UPPER STRINGER 12. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAP 57-10-05 FIG 5. (M)
- [SDR MZZA99214](https://openairdocs.org/sdr/MZZA99214.md): Stringer · cracked · Sep 28, 1999 · N15781 · Boeing 727232 · Wing, Longeron/Stringer
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON RIGHT WING UPPER STRINGER S-9 ATTACHED TO WS 629 RIB. THE CRACK WAS STOP DRILLED AND REPAIRED PER CMI EA NR 5762-01050. (M)
- [SDR MZZA99211](https://openairdocs.org/sdr/MZZA99211.md): Web · cracked · Sep 28, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, FOUR CRACKS WERE FOUND ON RIGHT LOWER TORQUE BOX VERTICAL WEB LIGHTENING HOLES BETWEEN BS 1223 AND BS 1243. THE CRACK WAS STOP DRILLED AND REPAIRED PER B727 SRM CHAPTER 51-40-02. (M)
- [SDR MZZA99189](https://openairdocs.org/sdr/MZZA99189.md): Fitting · cracked · Sep 28, 1999 · N15781 · Boeing 727232 · Auxiliary Gear (Tail Skid)
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON TAIL SKID ACTUATOR RIGHT HINGE ARM INBOARD SUPPORT BRACKET IN TAIL SKID BAY. THE CRACKED FITTING WAS REMOVED AND REPLACED WITH A NEW (P/N 65-57934-8) PER B727 SRM CHAPTER 51-10-01,
- [SDR MZZA99205](https://openairdocs.org/sdr/MZZA99205.md): Skin · cracked · Sep 23, 1999 · N15781 · Boeing 727232 · Fuselage Main, Plate/Skin
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 4 INCH LONG CRACK WAS FOUND ON FUSELAGE SKIN AT STRINGER 17R BETWEEN BS 730 AND BS 734. THE DAMAGED SECTION WAS TRIMMED AND REPAIRED PER CML ECRA NR 5330-2891. (M)
- [SDR MZZA99200](https://openairdocs.org/sdr/MZZA99200.md): Keel Beam · corroded · Sep 23, 1999 · N15781 · Boeing 727232 · Fuselage Main, Keel
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY.5 INCH AREA IG CORROSION WAS FOUND ON STRINGER29R KEEL BEAM OUTBOARD FLANGE AT BS 950 PLUS 14. THE CORRODED T-CHORD SECTION WAS TRIMMED AND REPAIRED PER B727 SB 53-0179. (M)
- [SDR MZZA99198](https://openairdocs.org/sdr/MZZA99198.md): Keel Beam · corroded · Sep 23, 1999 · N15781 · Boeing 727232 · Fuselage Main, Keel
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 3 INCH BY.5 INCH AREA CORROSION WAS FOUND S-29L KEEL BEAM OUTBOARD FLANGE AT BS 950 PLUS 14. THE CORRODED KEEL BEAM OUTBOARD FLANGE WAS TRIMMED AND REPAIRED PER B727 SB 53-0179. (M)
- [SDR MZZA99197](https://openairdocs.org/sdr/MZZA99197.md): Tee · corroded · Sep 23, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY 1 INCH AREA CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER T-CHORD AT RIGHT SIDE OF STRINGER 29R. THE CORRODED T-CHORD WAS TRIMMED AND REPAIRED PER CMI EC/RA NR 5310-3928. (M)
- [SDR MZZA99196](https://openairdocs.org/sdr/MZZA99196.md): Tee · corroded · Sep 23, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH LONG IG CORROSION WAS FOUND ON BS 950 BULKHEAD LOWER TEE CHORD BETWEEN STRINGER 29R AND S29L. THE CORRODED SECTION WAS TRIMMED AND REPAIRED PER B727 SRM CHAPTER 51-10-01 AND 51-30-02. (M)
- [SDR MZZA99193](https://openairdocs.org/sdr/MZZA99193.md): Fitting · cracked · Sep 23, 1999 · N15781 · Boeing 727232 · Cargo/Baggage Doors
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AIR ASIA, CRACK WAS FOUND ON C3 DOOR FORWARD LOWER CORNER STOP FITTING. THE DAMAGED STOP FITTING WAS REMOVED AND REPLACED WITH A NEW ONE (P/N 65-57768-6) PER CMI EA NR 5230-0185. (M)
- [SDR MZZA99192](https://openairdocs.org/sdr/MZZA99192.md): Skin · corroded · Sep 23, 1999 · N15781 · Boeing 727232 · Cargo/Baggage Doors
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 1.5 INCH LONG IG CORROSION WAS FOUND ON NR 3 CARGO DOOR FORWARD EDGE BETWEEN NR 3 AND NR 4 STOP FITTING. THE CORRODED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 51-40-03 FIG 1. (M)
- [SDR MZZA99225](https://openairdocs.org/sdr/MZZA99225.md): Control Cable · frayed · Sep 22, 1999 · N15781 · Boeing 727232 · Power Lever
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AIR ASIA, NR 1 ENGINE START CONTROL CABLE (ESS1A) WAS FOUND FRAYED AT BS 1186. THE FRAYED CABLE WAS REMOVED AND REPLACED PER B727 MM CHAPTER 76-12-01 AND OPERATIONAL CHECK FOUND NORMAL. (M)
- [SDR MZZA99217](https://openairdocs.org/sdr/MZZA99217.md): Spar · corroded · Sep 22, 1999 · N15781 · Boeing 727232 · Wing Spar
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, CORROSION OWAS FOUND ON LEFT WING FRONT SPAR WEB ABOVE FUEL BYPASS VALVE ACTUATOR. THE DAMAGED AREA WAS BLENDED OUT AND REPAIRED PER CMI EC/RA NR 5710-01978. (M)
- [SDR MZZA99213](https://openairdocs.org/sdr/MZZA99213.md): Spar · corroded · Sep 22, 1999 · N15781 · Boeing 727232 · Wing Spar
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A IG CORROSION WAS FOUND ON LEFT WING FRONT SPAR LOWER CHORD VERTICAL LEG AT FSS 401. THE CORRODED SECTION WAS CLEANED UP AND REPAIRED PER CMI EC/RA NR 5710-01975. (M)
- [SDR MZZA99212](https://openairdocs.org/sdr/MZZA99212.md): Skin · bulged · Sep 22, 1999 · N15781 · Boeing 727232 · Rudder, Plate/Skin
  > TNN - DURING D-CHECK INSPECTIN ON AIRCRAFT AT AIR ASIA, A 7 INCH BY 3 INCH AREA BULGE WAS FOUND ON UPPER RUDDER SKIN AT FIN STATION 270. THE DAMAGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-40-02, 55-20-03. (M)
- [SDR MZZA99210](https://openairdocs.org/sdr/MZZA99210.md): Skin · bulged · Sep 22, 1999 · N15781 · Boeing 727232 · Rudder, Plate/Skin
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A 2 INCH BY 4 INCH AREA BULGE WAS FOUND ON UPPER RUDDER SKIN AT FIN STATION 213. THE BULGED AREA WAS TRIMMED OUT AND REPAIRED PER B727 SRM CHAPTER 55-40-02 FIG 1 AND 55-20-03 FIG 1. (M)
- [SDR MZZA99209](https://openairdocs.org/sdr/MZZA99209.md): Beam · corroded · Sep 22, 1999 · N15781 · Boeing 727232 · Elevator 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 ELEV STAB 146. THE CORRODED AREA WAS REMOVED AND REPAIRED PER B727 SRM CHAP 55-10-06. (M)
- [SDR MZZA99202](https://openairdocs.org/sdr/MZZA99202.md): Fitting · cracked · Sep 20, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON AFT AIRSTAIR RIGHT LOWER STRUT END TO AIRSTAIR FITTING. THE CRACKED FITTING WAS REMOVED AND REPLACED WITH A NEW ONE (P/N 65-26651-18) PER B727 SRM CHAPTER 51-10-01. (M)
- [SDR MZZA99201](https://openairdocs.org/sdr/MZZA99201.md): Fitting · cracked · Sep 20, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > TNN - DURING D-CHECK INSPECTION ON AIRCRAFT AT AIR ASIA, A CRACK WAS FOUND ON AFT AIRSTAIR LEFT LOWER STRUT END TO AIRSTAIR FITTING. THE CRACKED FITTING WAS REMOVED AND REPLACED WITH A NEW ONE (P/N 65-26651-17) PER B727 SRM CHAPTER 51-10-01. (M)
- [SDR CALA9900629](https://openairdocs.org/sdr/CALA9900629.md): Skin · corroded · Jun 2, 1999 · N15781 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND THE NR 3 CARGO DOOR CUTOUT SKIN CORRODED AT AFT LOWER CORNER. REPAIRED IAW ECRA 5330-02818.
- [SDR CALA9900347](https://openairdocs.org/sdr/CALA9900347.md): Skin · cracked · Mar 31, 1999 · N15781 · Boeing 727232 · Fuselage Main, Plate/Skin
  > INSPECTION FOUND A 9 INCH CRACK IN FUSELAGE SKIN JUST UNDER FORWARD END OF NR 3 ENGINE PYLON. REPAIRED IAW SRM 53-30-3, FIGURE 3 SHEET 1.
- [SDR CALA9900322](https://openairdocs.org/sdr/CALA9900322.md): Skin · cracked · Mar 25, 1999 · N15781 · Boeing 727232 · Fuselage Main, Plate/Skin
  > AN INSPECTION OF THE LOWER SKIN OUTER SURFACE ALONG THE LOWEST ROW AT STRINGER 4R LAP SPLICE FROM BS 681 TO BS 740 FOUND CRACKS IN THE ENTIRE LENGTH OF THE PANEL. THE CRACKS MEASURED FROM.0625 INCH TO.25 INCH LONG. THE AREA WAS REPAIRED IAW ECRA 5330-02785
- [SDR CALA9900246](https://openairdocs.org/sdr/CALA9900246.md): Accessory Unit · inop · Mar 12, 1999 · N15781 · Boeing 727232 · Landing Gear Position and Warning
  > BOTH RT MLG RED AND GREEN ANNUNCIATOR LIGHTS ILLUMINATED DURING DESCENT. THE GEAR HANDLE WAS CYCLED FROM UP TO OFF AND THE GEAR DOOR LIGHT CAME ON. WHEN GEAR WAS SELECTED TO DOWN, GOT THREE GREEN AND LANDING WAS NORMAL. THE LANDING GEAR AND DOORS WERE INSPE
- [SDR CALA9900110](https://openairdocs.org/sdr/CALA9900110.md): Actuator · inoperative · Feb 5, 1999 · N15781 · Boeing 727232 · Landing Gear Door Actuator
  > THE LT MLG DOOR WOULD NOT RETRACT AFTER TAKEOFF FROM SFO. THE AIRCRAFT WAS RETURNED TO SFO WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT MLG DOOR ACTUATOR IAW MM 32-32-81. LEAK AND OPERATIONAL CHECKS WERE GOOD.
- [SDR CALA9800737](https://openairdocs.org/sdr/CALA9800737.md): Compressor · stalled · May 3, 1998 · N15781 · Boeing 727232 · Turbine Engine Compressor Section
  > AS AIRCRAFT LEVELING AT FL 350 THE POWER REDUCTION CAUSED HEAVY COMPRESSOR STALLS IN THE NUMBER ONE ENGINE. LARGE FLUCTUATION IN N1, EGT, N2, AND FUEL FLOW. RAN NR 1 ENGINE PER MM 71-00-87 TO TAKEOFF POWER FOR THREE MINUTES, REDUCED POWER. NO STALLS NOTICED
- [SDR CALA9800677](https://openairdocs.org/sdr/CALA9800677.md): Spar · corroded · Apr 17, 1998 · N15781 · Boeing 727232 · Vertical Stabilizer, Spar/Rib
  > INSPECTION FOUND VERTICAL STABILIZER FRONT SPAR FIN STA 87 TO 100 CORRODED ON RT SIDE. THE CORRODED AREA WAS CUT OUT, A REPAIR ANGLE AND STRAP WERE FABRICATED AND INSTALLED IAW ENGINEERING ORDER 98-833.
- [SDR CALA9800676](https://openairdocs.org/sdr/CALA9800676.md): Chord · corroded · Apr 15, 1998 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND AFT CARGO THRESHOLD LOWER CHORD CORRODED AT FS 950E TO 1010. THE AREA WAS REPAIRED IAW ECRA 5310-03710.

Next page: https://openairdocs.org/deregistered/N15781-2018-02-28/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 = 'N15781' AND deregistration_id = 'N15781-2018-02-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N15781-2018-02-28/reports

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