N15781, cancelled Feb 28, 2018

Service difficulty reports · 101

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR MZZA00002Battery · inoperativeGUM - 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)Jan 24, 2000 · N15781 · Boeing 727232 · Emergency LightingSDR MZZA99239Housing · crackedGUM - 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)Dec 24, 1999 · N15781 · Boeing 727232 · Landing Gear Retraction/Extension SystemSDR MZZA99199T-Chord · corrodedTNN - 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)Oct 26, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99226Control Cable · frayedTNN - 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)Oct 17, 1999 · N15781 · Boeing 727232 · Power LeverSDR MZZA99223Frame · corrodedTNN - 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)Oct 12, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99190Fitting · corrodedTNN - 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.Oct 11, 1999 · N15781 · Boeing 727232 · Auxiliary Gear (Tail Skid)SDR MZZA99224Tee · corrodedTNN - 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)Oct 8, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99206Floorbeam · crackedTNN - 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)Oct 6, 1999 · N15781 · Boeing 727232 · Fuselage Main, Floor BeamSDR MZZA99203Floorbeam · crackedTNN - 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)Oct 6, 1999 · N15781 · Boeing 727232 · Fuselage Main, Floor BeamSDR MZZA99195Stiffener · crackedTNN - 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 Oct 6, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99194Stiffener · crackedTNN - 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 6Oct 6, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99220Frame · crackedTNN - 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 65C34Oct 5, 1999 · N15781 · Boeing 727232 · Fuselage Main, FrameSDR MZZA99208Bracket · corrodedTNN - 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)Oct 5, 1999 · N15781 · Boeing 727232 · Passenger/Crew DoorsSDR MZZA99207Web · corrodedTNN - 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)Oct 5, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99228Stiffener · corrodedTNN - 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)Oct 4, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99227Stiffener · corrodedTNN - 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)Oct 4, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99204Frame · crackedTNN - 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. (MSep 29, 1999 · N15781 · Boeing 727232 · Fuselage Main, FrameSDR MZZA99191Skin · damagedTNN - 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)Sep 29, 1999 · N15781 · Boeing 727232 · Passenger/Crew DoorsSDR MZZA99222Web · crackedTNN - 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)Sep 28, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99221Gusset · corrodedTNN - 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)Sep 28, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99219Fitting · crackedTNN - 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)Sep 28, 1999 · N15781 · Boeing 727232 · Wing Miscellaneous StructureSDR MZZA99218Gusset · corrodedTNN - 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 51-10-01Sep 28, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99216Stringer · crackedTNN - 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)Sep 28, 1999 · N15781 · Boeing 727232 · Wing, Longeron/StringerSDR MZZA99215Rib · crackedTNN - 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)Sep 28, 1999 · N15781 · Boeing 727232 · Wing, Rib/BulkheadSDR MZZA99214Stringer · crackedTNN - 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)Sep 28, 1999 · N15781 · Boeing 727232 · Wing, Longeron/StringerSDR MZZA99211Web · crackedTNN - 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)Sep 28, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99189Fitting · crackedTNN - 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, Sep 28, 1999 · N15781 · Boeing 727232 · Auxiliary Gear (Tail Skid)SDR MZZA99205Skin · crackedTNN - 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)Sep 23, 1999 · N15781 · Boeing 727232 · Fuselage Main, Plate/SkinSDR MZZA99200Keel Beam · corrodedTNN - 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)Sep 23, 1999 · N15781 · Boeing 727232 · Fuselage Main, KeelSDR MZZA99198Keel Beam · corrodedTNN - 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)Sep 23, 1999 · N15781 · Boeing 727232 · Fuselage Main, KeelSDR MZZA99197Tee · corrodedTNN - 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)Sep 23, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99196Tee · corrodedTNN - 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)Sep 23, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99193Fitting · crackedTNN - 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)Sep 23, 1999 · N15781 · Boeing 727232 · Cargo/Baggage DoorsSDR MZZA99192Skin · corrodedTNN - 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)Sep 23, 1999 · N15781 · Boeing 727232 · Cargo/Baggage DoorsSDR MZZA99225Control Cable · frayedTNN - 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)Sep 22, 1999 · N15781 · Boeing 727232 · Power LeverSDR MZZA99217Spar · corrodedTNN - 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)Sep 22, 1999 · N15781 · Boeing 727232 · Wing SparSDR MZZA99213Spar · corrodedTNN - 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)Sep 22, 1999 · N15781 · Boeing 727232 · Wing SparSDR MZZA99212Skin · bulgedTNN - 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)Sep 22, 1999 · N15781 · Boeing 727232 · Rudder, Plate/SkinSDR MZZA99210Skin · bulgedTNN - 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)Sep 22, 1999 · N15781 · Boeing 727232 · Rudder, Plate/SkinSDR MZZA99209Beam · corrodedTNN - 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)Sep 22, 1999 · N15781 · Boeing 727232 · Elevator StructureSDR MZZA99202Fitting · crackedTNN - 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)Sep 20, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR MZZA99201Fitting · crackedTNN - 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)Sep 20, 1999 · N15781 · Boeing 727232 · Fuselage Miscellaneous StructureSDR CALA9900629Skin · corrodedINSPECTION FOUND THE NR 3 CARGO DOOR CUTOUT SKIN CORRODED AT AFT LOWER CORNER. REPAIRED IAW ECRA 5330-02818.Jun 2, 1999 · N15781 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9900347Skin · crackedINSPECTION 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.Mar 31, 1999 · N15781 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9900322Skin · crackedAN 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 5330-02785Mar 25, 1999 · N15781 · Boeing 727232 · Fuselage Main, Plate/SkinSDR CALA9900246Accessory Unit · inopBOTH 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 INSPEMar 12, 1999 · N15781 · Boeing 727232 · Landing Gear Position and WarningSDR CALA9900110Actuator · inoperativeTHE 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.Feb 5, 1999 · N15781 · Boeing 727232 · Landing Gear Door ActuatorSDR CALA9800737Compressor · stalledAS 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 NOTICEDMay 3, 1998 · N15781 · Boeing 727232 · Turbine Engine Compressor SectionSDR CALA9800677Spar · corrodedINSPECTION 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.Apr 17, 1998 · N15781 · Boeing 727232 · Vertical Stabilizer, Spar/RibSDR CALA9800676Chord · corrodedINSPECTION FOUND AFT CARGO THRESHOLD LOWER CHORD CORRODED AT FS 950E TO 1010. THE AREA WAS REPAIRED IAW ECRA 5310-03710.Apr 15, 1998 · N15781 · Boeing 727232 · Fuselage Miscellaneous Structure
Back to N15781, cancelled Feb 28, 2018