# Service difficulty reports: N578PE, cancelled Oct 24, 2002 A list on [N578PE, cancelled Oct 24, 2002](https://openairdocs.org/deregistered/N578PE-2002-10-24.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 · 54 reports - [SDR CALA9800137](https://openairdocs.org/sdr/CALA9800137.md): Bracket · cracked · Jan 29, 1998 · N578PE · Boeing 727243 · Leading Edge Slat Actuator > INSPECTION FOUND, A.75 INCH CRACK IN LT WING NR 2 LEADING EDGE FLAP ACTUATOR INBOARD ATTACH BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-3, 51-10-1, AND 51-30-2. - [SDR CALA9800136](https://openairdocs.org/sdr/CALA9800136.md): Bracket · cracked · Jan 29, 1998 · N578PE · Boeing 727243 · Leading Edge Slat Actuator > INSPECTION FOUND A.75 IN H CRACK IN LT WING NR 1 LEADING EDGE FLAP ACTUATOR ATTACH BRACKET. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-2. - [SDR CALA9800135](https://openairdocs.org/sdr/CALA9800135.md): Angle · cracked · Jan 29, 1998 · N578PE · Boeing 727243 · Leading Edge Devices > INSPECTION FOUND, A 2.25 INCH AND 1.5 INCH CRACK AT INBOARD UPSTOP AREA BELOW TELESCOPING ANTI-ICE DUCT OF LT WING NR 2 SLAT CHORD ANGLE. THE ANGLE WAS REPAIRED IAW SRM 51-40-3. - [SDR CALA9800715](https://openairdocs.org/sdr/CALA9800715.md): Wire · damaged · Jan 28, 1998 · N578PE · Boeing 727243 · Light System Wiring > INSPECTION FOUND FORWARD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE FOUND A DAMAGED WIRE AT CONNECTOR. THE WIRE WAS REPAIRED, THE LIGHT WAS RELAMPED, AND THE BATTERY PACK WAS RECHARGED. OPERATION CHECKED GOOD IAW MM 33-50. - [SDR CALA9800125](https://openairdocs.org/sdr/CALA9800125.md): Battery Pack · discharged · Jan 27, 1998 · N578PE · Boeing 727243 · Emergency Lighting > THE EMERGENCY LIGHTING AT MID CABIN CEILING EXIT LIGHT, COCKPIT DOOR EXIT LIGHT, AND L-1 AND R-1 LOWER EXIT LIGHTS FAILED CAPACITANCE TEST. THE BATTERY PACK WAS REMOVED AND REPLACED. - [SDR CALA9800124](https://openairdocs.org/sdr/CALA9800124.md): Battery Pack · discharged · Jan 27, 1998 · N578PE · Boeing 727243 · Emergency Lighting > THE EMERGENCY PATH LIGHTING AT FIRST CLASS SECTION AND ROWS 17 TO 22 FAILED CAPACITANCE TEST. TWO BATTERY PACKS WERE REMOVED AND REPLACED. - [SDR CALA9800123](https://openairdocs.org/sdr/CALA9800123.md): Angle · cracked · Jan 27, 1998 · N578PE · Boeing 727243 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1.5 INCH CRACK IN AFT STAIRS ACTUATOR ATTACH ANGLES AT STA 1263 INSIDE RT TORQUE BULKHEAD. NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1. - [SDR CALA9800122](https://openairdocs.org/sdr/CALA9800122.md): Bracket · cracked · Jan 27, 1998 · N578PE · Boeing 727243 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1 INCH CRACK ON AFT SIDE OF AFT AIRSTAIRS ACTUATOR ATTACH BULKHEAD SUPPORT BRACKET AT STA 1263. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1. - [SDR CALA9800121](https://openairdocs.org/sdr/CALA9800121.md): Angle · cracked · Jan 27, 1998 · N578PE · Boeing 727243 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1 INCH CRACK IN FORWARD SUPPORT ANGLE OF AFT AIRSTAIRS RT SIDE STA 1273 (TORQUE BOX). ALSO, A 1 INCH CRACK WAS FOUND IN UPPER ANGLE OF AFT SIDE OF BULKHEAD IN AFT AIRSTAIR AREA ON RT SIDE AT STA 1273. NEW ANGLES WERE FABRICATED AND INSTALL - [SDR CALA9800120](https://openairdocs.org/sdr/CALA9800120.md): Bracket · cracked · Jan 27, 1998 · N578PE · Boeing 727243 · Leading Edge Slat Actuator > INSPECTION FOUND A 3 INCH CRACK IN INBOARD MOUNT BRACKET WHERE NR 1 SLAT ACTUATOR MOUNTS. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-1 AND 51-30-2. - [SDR CALA9800119](https://openairdocs.org/sdr/CALA9800119.md): Skin · cracked · Jan 27, 1998 · N578PE · Boeing 727243 · Wing, Plate/Skin > INSPECTION FOUND A.1875 INCH CRACK IN LT WING TRAILING EDGE UPPER SKIN AT NR 3 SPOILER THIRD CUTOUT FROM INBOARD HINGE. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-4 AND 51-10-2. - [SDR CALA9800118](https://openairdocs.org/sdr/CALA9800118.md): Skin · cracked · Jan 27, 1998 · N578PE · Boeing 727243 · Wing, Plate/Skin > INSPECTION FOUND A.25 INCH CRACK IN LT WING TRAILING EDGE UPPER SKIN AT NR 3 SPOILER SECOND CUTOUT FROM INBOARD HINGE. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-4 AND 51-30-2. - [SDR CALA9800117](https://openairdocs.org/sdr/CALA9800117.md): Stringer · cracked · Jan 27, 1998 · N578PE · Boeing 727243 · Wing, Longeron/Stringer > INSPECTION FOUND A.5 INCH CRACK IN VENT BOX STRINGER INSIDE LT WING TANK ACCESS 7217, WS 656.50. A REPAIR WAS INSTALLED IAW EA 5712-01050. - [SDR CALA9800116](https://openairdocs.org/sdr/CALA9800116.md): Angle · cracked · Jan 27, 1998 · N578PE · Boeing 727243 · Wing Miscellaneous Structure > INSPECTION FOUND A 2 INCH CRACK THROUGH TWO FASTENER HOLES OF RIB SUPPORT ANGLE AT WING LEADING EDGE SLAT STA 0. THE RIB SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1. - [SDR CALA9800115](https://openairdocs.org/sdr/CALA9800115.md): Skin · cracked · Jan 27, 1998 · N578PE · Boeing 727243 · Leading Edge Devices > INSPECTION FOUND A.375 INCH CRACK IN LT WING NR 4 SLAT LOWER SKIN JUST OUTBOARD OF INBOARD TRACK AREA. THE CRACKED AREA WAS BLENDED OUT. A PATCH REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-50-1, 51-10-2, AND 57-50-3. - [SDR CALA9800114](https://openairdocs.org/sdr/CALA9800114.md): Angle · cracked · Jan 27, 1998 · N578PE · Boeing 727243 · Wing Miscellaneous Structure > INSPECTION FOUND A 6 INCH CRACK AT FASTENERS IN SUPPORT ANGLE INSIDE LT WING INBOARD LEADING EDGE AREA AFT OF NR 1 LEADING EDGE FLAP INBOARD END AT L/E STA 130. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1. - [SDR CALA9800113](https://openairdocs.org/sdr/CALA9800113.md): Skin · cracked · Jan 27, 1998 · N578PE · Boeing 727243 · Wing, Plate/Skin > INSPECTION FOUND A.625 INCH CRACK IN LT WING UPPER FIXED LEADING EDGE SKIN WHERE NR 3 SLAT OUTBOARD HOOK ATTACHES. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1. DOUBLER, BACK STRAP, AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 57-30-4 AND 51-10-2. - [SDR CALA9800112](https://openairdocs.org/sdr/CALA9800112.md): Floorbeam · corroded · Jan 27, 1998 · N578PE · Boeing 727243 · Fuselage Main, Floor Beam > INSPECTION FOUND FLOORBEAM CORRODED ON AND AROUND NUT PLATES IN E AND E COMPARTMENT UNDER GALLEY AT STA 380. THE CORRODED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-8, 51-10-4, AND 51-10-1. - [SDR CALA9800111](https://openairdocs.org/sdr/CALA9800111.md): Angle · corroded · Jan 27, 1998 · N578PE · Boeing 727243 · Fuselage Miscellaneous Structure > INSPECTION FOUND Z-ANGLE CORRODED AT STA 616 ABOVE STRINGER 26R IN FORWARD BAGGAGE BIN. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. - [SDR CALA9800110](https://openairdocs.org/sdr/CALA9800110.md): Support · corroded · Jan 27, 1998 · N578PE · Boeing 727243 · Fuselage Miscellaneous Structure > INSPECTION FOUND RT FLOOR SUPPORT IN FORWARD BAGGAGE BIN CORRODED FROM DTA 616 TO 660. THE FLOOR SUPPORT WAS REMOVED AND A NEW SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. - [SDR CALA9800109](https://openairdocs.org/sdr/CALA9800109.md): Skin · dented · Jan 27, 1998 · N578PE · Boeing 727243 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1030 BETWEEN STRINGERS 20-21L. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 AND 51-10-6. - [SDR CALA9701235](https://openairdocs.org/sdr/CALA9701235.md): Prbc · broken · Aug 23, 1997 · N578PE · Boeing 727243 · Compressor Bleed Valve > THE NR 3 ENGINE EGT HIT REDLINE ON TAKEOFF ROLL. REDUCING EPR TO 1.4 FAILED TO KEEP EGT OUT OF REDLINE. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND FITTING ON PRBC BROKEN. THE PRBC WAS REPLACED IAW MM 75-31-13. THE - [SDR CALA9701189](https://openairdocs.org/sdr/CALA9701189.md): Lock Actuator · inoperative · Aug 12, 1997 · N578PE · Boeing 727243 · Landing Gear Retraction/Extension System > THE NOSE GEAR DID NOT EXTEND WHEN GEAR HANDLE WAS SELECTED DOWN ON FINAL APPROACH. THE GEAR WAS CYCLED AND EXTENDED NORMALLY FOR A SAFE LANDING AT IAH. MAINTENANCE FOUND THE NLG LOCK ACTUATOR AT FAULT. THE NLG LOCK ACTUATOR WAS REMOVED AND REPLACED IAW MM 3 - [SDR CALA9701156](https://openairdocs.org/sdr/CALA9701156.md): Actuator · inoperative · Aug 1, 1997 · N578PE · Boeing 727243 · Landing Gear Door Actuator > THE RT MLG WOULD NOT RETRACT WHEN GEAR HANDLE WAS PLACED IN THE UP POSITION AFTER TAKEOFF. THE SECOND OFFICER'S ANNUNCIATOR PANEL INDICATED THAT THE RIGHT GEAR DOOR WAS DOWN. A VISUAL CHECK CONFIRMED THE GEAR WAS DOWN. THE AIRCRAFT WAS RETURNED TO IAH WHERE - [SDR CALA9700820](https://openairdocs.org/sdr/CALA9700820.md): Hyd Line · leaking · Jun 4, 1997 · N578PE · Boeing 727243 · Hydraulic System, Main > THE 'A' SYSTEM HYDRAULIC FLUID WAS LOST WHEN LANDING GEAR WAS RAISED AFTER TAKEOFF FROM MCO. THE AIRCRAFT WAS RETURNED TO MCO WHERE IT LANDED WITHOUT INCIDENT. MX FOUND THE LT MLG DOOR ACTUATOR PRESSURE LINE LEAKING. THE PRESSURE LINE WAS REMOVED AND REPLAC - [SDR CALA9700311](https://openairdocs.org/sdr/CALA9700311.md): Actuator · failed · Mar 5, 1997 · N578PE · Boeing 727243 · Landing Gear Door Actuator > THE A-HYDRAULIC SYSTEM QUANTITY WAS LOST WHEN GEAR WAS EXTENDED FOR LANDING ON APPROACH. CHECKLIST PROCEDURES WERE COMPLIED WITH AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE LT MLG DOOR RETRACT AND EXTEND ACTUATOR FAILED. THE ACTUATOR WAS - [SDR CALA9700177](https://openairdocs.org/sdr/CALA9700177.md): Skin · cracked · Feb 2, 1997 · N578PE · Boeing 727243 · Wing, Plate/Skin > INSPECTION FOUND A.5 INCH CRACK IN CUTOUT FOR NR 3 LEADING EDGE SLAT INBOARD TRACK, LT WING. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-4. - [SDR CALA9601767](https://openairdocs.org/sdr/CALA9601767.md): Control Module · inoperative · Dec 9, 1996 · N578PE · Boeing 727243 · Elevator Control System > THE AIRCRAFT LOST A-SYSTEM HYDRAULIC PRESSURE AND QUANTITY APPROXIMATELY 10 MINUTES AFTER TAKEOFF. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE A-SYSTEM ELEVATOR CONTROL MODULE AT FAULT. THE ELEVATOR CONTROL MODULE WAS REPLACED. THE NR 1 ENG - [SDR CALA9600828](https://openairdocs.org/sdr/CALA9600828.md): Frame · damaged · Jun 12, 1996 · N578PE · Boeing 727243 · Fuselage Main, Frame > INSPECTION FOUND IMPACT DAMAGE TO FRAMES AT STA 169.8 AND 211.5, WL 170. THE FRAMES WERE REPAIRED IAW SRM 51-40-4, FIGURE 3. - [SDR CALA9600772](https://openairdocs.org/sdr/CALA9600772.md): Skin · punctured · Jun 8, 1996 · N578PE · Boeing 727243 · Fuselage Main, Plate/Skin > INSPECTION FOUND TWO SMALL HOLES IN FUSELAGE SKIN DUE TO GROUND DAMAGE AT STA 196 AND 211.5, RT SIDE. AN INTERIM REPAIR WAS INSTALLED IAW SRM 53-30-3, FIGURE 1, PAGE 5. A DIP WAS ISSUED TO INSPECT REPAIR EVERY 3,000 FLIGHTS AND TO PERFORM A PERMANENT REPAIR - [SDR CAL960015](https://openairdocs.org/sdr/CAL960015.md): Skin · cracked · Dec 28, 1995 · N578PE · Boeing 727243 · Passenger/Crew Doors > INSPECTION FOUND A.50 INCH CRACK IN L-1 DOOR INTERNAL SKIN AT TORQUE BOX CUT OUT. THE CRACKED AREA WAS BLENDED OUT. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 52-00-2, SRM 51-10-1, AND SRM 51-20-4. (X) - [SDR CAL960034](https://openairdocs.org/sdr/CAL960034.md): Stringer · corroded · Dec 26, 1995 · N578PE · Boeing 727243 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND STR 29R CORRODED AT SPLICE AND UNDER LEVELING COMPOUND AT CENTER OF STRINGER IN AFT CARGO BIN BS 1000. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A STRINGER SPLICE AND REPAIR DOUBLER ANGLE WERE FABRICATED AND INSTALLED IAW SRM 51-10-1 AND SR - [SDR CAL960035](https://openairdocs.org/sdr/CAL960035.md): Stringer · corroded · Dec 18, 1995 · N578PE · Boeing 727243 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND STR 29L CORRODED AT STA 972 IN AFT PIT. THE CORROSION WAS BLENDED OUT IAW SRM 51-10-6. A REPAIR STRAP WAS FABRICATED AND INSTALLED IAW ECRA 5310-03205. (X) - [SDR CAL960027](https://openairdocs.org/sdr/CAL960027.md): Strap · corroded · Dec 18, 1995 · N578PE · Boeing 727243 · Fuselage Miscellaneous Structure > INSPECTION FOUND DOUBLER STRAP CORRODED AROUND C-1 ENTRANCE AT STA 560 ABOVE STR 26R. THE CORROSION WAS REMOVED IAW SRM 51-10-6, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW ECRA 5230-01298 AND SRM 51-30-2. (X) - [SDR CAL960022](https://openairdocs.org/sdr/CAL960022.md): Support · corroded · Dec 18, 1995 · N578PE · Boeing 727243 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD CARGO FLOOR SUPPORT STRUCTURE AT STA 640 CENTER SECTION CORRODED. THE CORROSION WAS REMOVED IAW SRM 51-10-6, AN 'L' ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-4 AND SRM 53-10-8. (X) - [SDR CAL960036](https://openairdocs.org/sdr/CAL960036.md): Stringer · corroded · Dec 15, 1995 · N578PE · Boeing 727243 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND STR 28L CORRODED BETWEEN STA 985 AND STA 994, IN THE AFT PIT. THE CORRODED SECTION WAS REMOVED AND A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND MM 51-40-5. (X) - [SDR CAL9690026](https://openairdocs.org/sdr/CAL9690026.md): Stringer · corroded · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND STR 26R CORRODED AT STA 520 - STA 560. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, SRM 53-10-1, SRM 51-10-2, SRM 51-30-2, AND SRM 51-40-5. (X) - [SDR CAL960040](https://openairdocs.org/sdr/CAL960040.md): Bulkhead Fitting · corroded · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Main, Bulkhead > INSPECTION FOUND CORROSION IN FORWARD CARGO BS 740 BULKHEAD FITTING AT S28L. THE CORROSION WAS CLEANED AND TREATED IAW SRM 51-10-2. L-ANGLE SPLICE WAS FABRICATED AND INSTALLED IAW SRM'S 51-30-2, 53-10-3, 51-10-2, AND 51-20-4. (X) - [SDR CAL960039](https://openairdocs.org/sdr/CAL960039.md): Bulkhead Fitting · corroded · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Main, Bulkhead > INSPECTION FOUND CORROSION IN FORWARD CARGO BS 740 BULKHEAD CORNER FITTING AT S28R. A NEW STRINGER SECTION AND REPAIR SPLICE WERE INSTALLED IAW SRM 51-30-2, SRM 53-10-3, AND ECRA 5340-01256. (X) - [SDR CAL960038](https://openairdocs.org/sdr/CAL960038.md): Frame · corroded · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Main, Frame > INSPECTION FOUND UPPER SURFACE OF BELT FRAME LOWER FLANGE IN AFT CARGO BIN CORRODED AT BS 990, LBL 16. THE CORROSION WAS REMOVED IAW SRM 51-10-6. (X) - [SDR CAL960037](https://openairdocs.org/sdr/CAL960037.md): Shear Tie · corroded · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Miscellaneous Structure > INSPECTION FOUND SHEAR TIE CORRODED AT FS 990 BETWEEN STR 28L AND STR 29L. THE CORROSION WAS REMOVED IAW SRM 51-10-6. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM'S 53-10-4, 51-10-1, 51-10-2, AND 51-30-2. (X) - [SDR CAL960030](https://openairdocs.org/sdr/CAL960030.md): Stringer · corroded · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND STR 27L CORRODED IN AFT CARGO COMPARTMENT AT BS 1015. THE CORRODED SECTION OF STRINGER WAS REMOVED IAW SRM 51-30-2. A STRINGER REPAIR AND HAT SECTION WAS FABRICATED AND INSTALLED IAW SRM 53-10-3 AND SRM 51-30-2. (X) - [SDR CAL960029](https://openairdocs.org/sdr/CAL960029.md): Shear Tie · corroded · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Miscellaneous Structure > INSPECTION FOUND SHEAR TIE CORRODED BETWEEN S27R AND S28R AND STA 1010. A SHEAR TIE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4, SRM 51-10-2, AND SRM 51-30-2. (X) - [SDR CAL960028](https://openairdocs.org/sdr/CAL960028.md): Stringer · corroded · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Main, Longeron/Stringer > INSPECTION FOUND STRINGER 26R CORRODED AT STA 1166. THE STRINGER WAS REMOVED AND A NEW STRINGER WAS FABRICATED AND INSTALLED IAW SRM 53-10-3. (X) - [SDR CAL960025](https://openairdocs.org/sdr/CAL960025.md): Frame · cracked · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FORWARD CARGO FRAME AT STA 580 AND CENTER OF FLOOR STRUCTURE. THE CRACKED AREA WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-10-1, SRM 51-10-2, AND SRM 51-30-2. (X) - [SDR CAL960024](https://openairdocs.org/sdr/CAL960024.md): Support · corroded · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD CARGO RIGHT FLOOR SUPPORT STRUCTURE CORRODED AT BS 480 - BS 560. A REPAIR PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-40-2, SRM 53-10-1, AND SRM 51-30-2. (X) - [SDR CAL960023](https://openairdocs.org/sdr/CAL960023.md): Frame · cracked · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Main, Frame > INSPECTION FOUND FORWARD CARGO FRAME STA 640 CRACKED AT S29R (.50 INCH), S29L (1.5 INCHES), AND S28L (.25 INCH). A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, SRM 51-30-5, SRM 51-10-2, AND SRM 51-30-2. (X) - [SDR CAL960020](https://openairdocs.org/sdr/CAL960020.md): Frame · cracked · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Main, Frame > INSPECTION FOUND A.3750 INCH CRACK IN FORWARD CARGO FRAME AT STA 660, STR 28R. A REPAIR DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 53-10-4 AND SRM 51-30-2. (X) - [SDR CAL960018](https://openairdocs.org/sdr/CAL960018.md): Frame · cracked · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Main, Frame > INSPECTION FOUND A.25 INCH CRACK IN FORWARD CARGO FRAME AT STA 600 AND CENTER FLOOR STRUCTURE. THE CRACKED SECTION OF FRAME WAS CUT OUT IAW SRM 51-40-3. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND SRM 51-30-2. (X) - [SDR CAL960017](https://openairdocs.org/sdr/CAL960017.md): Frame · cracked · Dec 14, 1995 · N578PE · Boeing 727243 · Fuselage Main, Frame > INSPECTION FOUND A 2.5 INCH CRACK IN FORWARD CARGO FRAME AT STA 720, LBL 6. THE CRACKED SECTION OF FRAME WAS CUT OUT. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, SRM 51-10-1, SRM 51-10-2, AND SRM 51-30-2. (X) Next page: https://openairdocs.org/deregistered/N578PE-2002-10-24/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 = 'N578PE' AND deregistration_id = 'N578PE-2002-10-24' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N578PE-2002-10-24/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.