# Service difficulty reports: N79748, cancelled May 4, 2011 A list on [N79748, cancelled May 4, 2011](https://openairdocs.org/deregistered/N79748-2011-05-04.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 · 107 reports - [SDR GAIA04047OP](https://openairdocs.org/sdr/GAIA04047OP.md): Control Column · binding · Mar 9, 2004 · N79748 · Boeing 727224 · Control Column Section > DURING CRUISE FLIGHT, A BINDING OF THE CONTROL YOKE WAS NOTED IN A ROLL TO THE RIGHT. SPOILERS WERE CYCLED AND ABOVE PROBLEM WAS CORRECTED BUT LATER DID RETURN. FLT WAS COMPLETED AND AN UNEVENTFUL LANDING WAS MADE. INSPECTED AND CHECK FLIGHT CONTROLS AILERO - [SDR GAIA04037OP](https://openairdocs.org/sdr/GAIA04037OP.md): Computer · malfunctioned · Feb 25, 2004 · N79748 · Boeing 727224 · Autopilot Computer > FLT 578 - SFO-PHX-FWA - AUTOPILOT DIFFICULT TO ENGAGE IN CRUISE. REMOVED AND REPLACED THE PITCH CHANNEL COMPUTER. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA04024OP](https://openairdocs.org/sdr/GAIA04024OP.md): Fire Loop · loose · Feb 19, 2004 · N79748 · Boeing 727224 · Fire Detection > THE NR 3 ENGINE GROUND FAULT LIGHT CAME ON DURING TAXI AT SFO. INSPECTED AND CHECKED NR 3 ENGINE FIRE LOOP CLEANED AND RESECURED CONNECTORS. THE SYSTEM OPERATIONALLY CHECKED GOOD NO DEFECTS FOUND. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA03116OP](https://openairdocs.org/sdr/GAIA03116OP.md): Light · inoperative · Oct 25, 2003 · N79748 · Boeing 727224 · Emergency Lighting > DURING ROUTINE MAINTENANCE AT FWA, IT WAS DISCOVERED THAT THE MAIN ENTRY EMERGENCY EXIT LIGHT DID NOT ILLUMINATE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA03007OP](https://openairdocs.org/sdr/GAIA03007OP.md): Indicator · false indication · Feb 12, 2003 · N79748 · Boeing 727224 · Engine Oil Quantity > FLT 879 - RNO-SJC - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE OIL QUANTITY ON NR 2 ENGINE WAS STEADILY DECREASING. THE CREW DECLARED AN EMERGENCY AND MADE A PRECAUTIONARY SHUT DOWN OF THE NR 2 ENGINE. DURING APPROACH THE OIL QUANTITY RETURNED TO NORMAL - [SDR GAIA02100ST](https://openairdocs.org/sdr/GAIA02100ST.md): Hinge · cracked · Sep 4, 2002 · N79748 · Boeing 727224 · Cargo/Baggage Doors > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FORWARD MAIN CARGO DOOR HINGE WAS CRACKED. INSTALLED NEW HINGE SECTION PER AEI SERVICES BULLETIN 01-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA02093ST](https://openairdocs.org/sdr/GAIA02093ST.md): Frame · dented · Sep 3, 2002 · N79748 · Boeing 727224 · Fuselage Main, Frame > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME WAS DENTED JUST ABOVE FLOOR LEVEL RIGHT MAIN CARGO COMPARTMENT BS 600. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3 FIGURE 1, FABRICATED REPAIR DOUBLER IAW B727 SRM 51-40-3 AND 53-10 - [SDR GAIA02101ST](https://openairdocs.org/sdr/GAIA02101ST.md): Hinge · cracked · Sep 3, 2002 · N79748 · Boeing 727224 · Cargo/Baggage Doors > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE AFT MAIN CARGO DOOR HINGE WAS CRACKED. INSTALLED NEW HINGE SECTION AEI SERVICE BULLETIN 01-01. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA02081ST](https://openairdocs.org/sdr/GAIA02081ST.md): Door Frame · corroded · Sep 3, 2002 · N79748 · Boeing 727224 · Fuselage Main, Structure > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT AT THE E/E ACCESS, THE AFT DOOR LOCKING FRAME HAD CORROSION AT THE FRAME TO SKIN AT BS 460, STRINGER S29L TO S28L. REMOVED FRAME DAMAGE, AND REPAIRED PER BOEING SRM 51-10-2 FIGURE 3. THE AIRCRAFT WAS RETURN - [SDR GAIA02083ST](https://openairdocs.org/sdr/GAIA02083ST.md): Skin · dented · Sep 3, 2002 · N79748 · Boeing 727224 · Fuselage Main, Plate/Skin > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE EXTERIOR NOSE SECTION AT BS 310 THROUGH 330 BETWEEN STRINGERS 21R TO STRINGER 22R SKIN WAS DENTED. CUT OUT DAMAGED AREA. FABRICATED DOUBLER AND FILLER TREATED AND PRIMED AREA IAW SRM 53-30-3 FI - [SDR GAIA02085ST](https://openairdocs.org/sdr/GAIA02085ST.md): Stringer · cracked · Sep 3, 2002 · N79748 · Boeing 727224 · Fuselage Main, Longeron/Stringer > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT IN THE MAIN CARGO COMPARTMENT INTERIOR AT BS 720B HAD A CRACK AT STRINGER S15L FORWARD OF WING LIGHT SUPPORT. CUT OUT DAMAGED AREA, FABRICATED NEW PART IAW B727 SRM 53-10-3, FIG 5. THE AIRCRAFT WAS RETURNED - [SDR GAIA02086ST](https://openairdocs.org/sdr/GAIA02086ST.md): Stringer · cracked · Sep 3, 2002 · N79748 · Boeing 727224 · Fuselage Main, Longeron/Stringer > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE MAIN CARGO COMPARTMENT INTERIOR BS 720B HAD A CRACK AT STRINGER S15R END, FORWARD OF WING LIGHT SUPPORT. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED NEW PART IAW B727 SRM 53-10-3, FIGURE 5. THE AIRCRA - [SDR GAIA02091ST](https://openairdocs.org/sdr/GAIA02091ST.md): Frame · dented · Sep 3, 2002 · N79748 · Boeing 727224 · Fuselage Main, Frame > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME WAS DENTED JUST ABOVE FLOOR LEVEL AT THE RIGHT SIDE MAIN CARGO COMPARTMENT BS 560. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3, FIGURE 1. FABRICATED DOUBLER IAW B727-SRM 51-40-3, F - [SDR GAIA02092ST](https://openairdocs.org/sdr/GAIA02092ST.md): Frame · dented · Sep 3, 2002 · N79748 · Boeing 727224 · Fuselage Main, Frame > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME WAS DENTED JUST ABOVE FLOOR LEVEL AT THE RIGHT MAIN CARGO COMPARTMENT BS 580. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3, FIGURE 1. FABRICATED DOUBLER IAW B727 SRM 51-40-3 AND 53- - [SDR GAIA02090ST](https://openairdocs.org/sdr/GAIA02090ST.md): Frame · dented · Sep 3, 2002 · N79748 · Boeing 727224 · Fuselage Main, Frame > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE FRAME DENTED JUST ABOVE FLOOR LEVEL RIGHT CABIN BS 540. CUT OUT DAMAGED AREA OF FRAME IAW B727 SRM 51-40-3 FIGURE 1. FABRICATED DOUBLER IAW B727 SRM 51-40-3, FIGURE 1 AND 53-10-2 FIGURE 2. THE - [SDR GAIA02089ST](https://openairdocs.org/sdr/GAIA02089ST.md): Frame · cracked · Sep 3, 2002 · N79748 · Boeing 727224 · Fuselage Main, Frame > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE BS 360, FRAME INBOARD FLANGE WAS DENTED AND CRACKED IN THE AREA OF STRINGER 16 LEFT. CUT OUT DAMAGED AREA IAW B727 SRM 51-40-3, FIG 1 FABRICATED DOUBLER IAW B727 SRM 51-20-1 AND 51-40-3 FIG 1. THE AIRCA - [SDR GAIA02088ST](https://openairdocs.org/sdr/GAIA02088ST.md): Frame · dented · Sep 3, 2002 · N79748 · Boeing 727224 · Fuselage Main, Frame > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FORWARD CARGO COMPARTMENT, THE FRAME AT BS 680 HAS THREE DENTS INTO THE RADIUS OF STRINGERS S25L TO S23L. COLD WORKED DENTS, NDT FOUND NO CRACKS, FABRICATED DOUBLER REPAIR IAW B727 SRNM 51-40-3, FIGURE 1 - [SDR GAIA02087ST](https://openairdocs.org/sdr/GAIA02087ST.md): Plenum · corroded · Sep 3, 2002 · N79748 · Boeing 727224 · Wing, Plate/Skin > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT AFT PLENUM LOWER SKIN HAS CORROSION IN TWO PLACES. FOUND CORROSION OUT OF LIMITS. INSTALLED DOUBLER AND TRIPLER IAW B727 SRM 57-30-3 FIGURE 8. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA02084ST](https://openairdocs.org/sdr/GAIA02084ST.md): Skin · dented · Sep 3, 2002 · N79748 · Boeing 727224 · Fuselage Main, Plate/Skin > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THERE WAS A DENT IN THE SKIN AT BS 1130, STRINGER 27L. REMOVED OLD REPAIR CUT OUT DAMAGED AREA INSTALLED FILLER, DOUBLER AND TRIPLER PER BOEING SRM 53-30-3, FIGURE 5. THE AIRCRAFT WAS RETURNED TO SERVICE. - [SDR GAIA02082ST](https://openairdocs.org/sdr/GAIA02082ST.md): Skin · dented · Sep 3, 2002 · N79748 · Boeing 727224 · Fuselage Main, Plate/Skin > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THERE WAS A DENT IN THE SKIN AT BS 1090, STRINGER S15R. CUT OUT DAMAGED AREA FABRICATED DOUBLER IAW B727 SRM 53-30-3, FIGURE 1, SHEET 2, PATE 6. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA02080ST](https://openairdocs.org/sdr/GAIA02080ST.md): Skin · dented · Sep 3, 2002 · N79748 · Boeing 727224 · Fuselage Main, Plate/Skin > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE FORWARD LOWER CARGO DOOR CUTOUT FRAME AND SKIN WAS DENTED NEAR STRINGER S23R AT THE FORWARD PORTION OF THE DOOR CUTOUT FRAME (FUSELAGE SKIN). C/A: ACCOMPLISHED REPAIR IAW REPAIR ORDER. AIRCRAFT WAS RET - [SDR GAIA01314OP](https://openairdocs.org/sdr/GAIA01314OP.md): Frame · chafed · Nov 10, 2001 · N79748 · Boeing 727224 · Fuselage Main, Frame > FLT - 3850 - MSP-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE 'A' SYSTEM HYDRAULIC FLUID QUANTITY WAS DECREASING. AN EMERGENCY WAS DECLARED AND THE HYDRAULIC SYSTEM WAS ISOLATED THE AIRCRAFT CONTINUED TO FWA. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. - [SDR GAIA01313OP](https://openairdocs.org/sdr/GAIA01313OP.md): Hydraulic Line · cracked · Nov 10, 2001 · N79748 · Boeing 727224 · Hydraulic System, Main > FLT 3850 - MSP-FWA - DURING CRUISE, THE FLIGHT CREW NOTICED THAT THE 'A' SYSTEM HYDRAULIC SYSTEM WAS ISOLATED THE AIRCRAFT CONTINUED TO FWA. THE AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTION REVEALED A CRACKED HYDRAULIC LINE AT FUSELAGE STATION 1303. THE - [SDR GAIA01238ST](https://openairdocs.org/sdr/GAIA01238ST.md): Light · not seated · May 11, 2001 · N79748 · Boeing 727224 · Emergency Lighting > MAINTENANCE FOUND EMERGENCY EXIT LIGHTS INOPERATIVE. FOUND LIGHT ASSEMBLY NOT SEATED IN CONNECTOR. REINSTALLED AND OPERATIONALLY CHECKED SYSTEM. SYSTEM CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M) - [SDR GAIA01156OP](https://openairdocs.org/sdr/GAIA01156OP.md): Hydraulic Line · leaking · May 1, 2001 · N79748 · Boeing 727224 · Hydraulic System, Main > FLT 1850 - PDX-SEA - UPON LANDING GEAR EXTENSION, LOST A SYSTEM HYDRAULICS QUANTITY WENT TO ZERO. AIRCRAFT MADE AN UNEVENTFUL LANDING IN SEA. INSPECTION OF AIRCRAFT FOUND LEAKING LEFT GEAR DOOR ACTUATOR RETURN HOSE. REMOVED AND LEFT ACTUATOR RETURN HOSE. REM - [SDR GAIA01073BOP](https://openairdocs.org/sdr/GAIA01073BOP.md): Line · ruptured · Feb 23, 2001 · N79748 · Boeing 727224 · Hydraulic System, Main > FLT 1805 - FWA-LAX - AT FL310, HYDRAULIC SYSTEM ''A'' PRESSURE AND QUANTITY WENT TO ZERO. AIRCRAFT MADE AN UNEVENTFUL LANDING IN DEN. TROUBLESHOOT AND FOUND RUPTURED HYDRAULIC LINE IN RIGHT SIDE OF AFT AIRSTAIR. REMOVED AND REPLACED THE HYDRAULIC LINE PER B - [SDR GAIA00800](https://openairdocs.org/sdr/GAIA00800.md): Line · leaking · Dec 30, 2000 · N79748 · Boeing 727224 · Hydraulic System, Main > FLT 3712 - FWA-ELP - SYSTEM ''A'' HYDRAULIC PRESSURE AND QUANTITY DROPPED TO ZERO ON CLIMB-OUT. AIRCRAFT MADE AN UNEVENTFUL RETURN TO FWA. FOUND NR 2 ENGINE ''A'' SYSTEM RETURN LINE LEAKING. INSTALLED FLEX LINE AND PERFORMED ENGINE RUN. NO LEAKS NOTED AND - [SDR GAIA00688](https://openairdocs.org/sdr/GAIA00688.md): Light · inoperative · Nov 9, 2000 · N79748 · Boeing 727224 · Emergency Lighting > NO FLIGHT. DURING ROUTINE MAINTENANCE, DISCOVERED THE L-1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED GOOD. THE AIRCRAFT RETURNED TO SERVICE. (X) - [SDR GAIA00491](https://openairdocs.org/sdr/GAIA00491.md): Rod End · sheared · Aug 7, 2000 · N79748 · Boeing 727224 · Steering Unit > DISCREPANCY: TAKE OFF ABORTED AT 70 KTS DUE TO VIOLENT NOSE WHEEL SHIMMY.CORRECTIVE ACTION: FOUND NOSE GEAR TORQUE LINKS TO BE DISCONNECTED CAUSING EXCESSIVE SHIMMY, RE-CONNECTED AS REQUIRED. UPON FURTHER INSPECTION FOUND NOSE WHEEL STEERING BYPASS LINKAGE ROD - [SDR GAIA00125](https://openairdocs.org/sdr/GAIA00125.md): Light · inoperative · Mar 30, 2000 · N79748 · Boeing 727224 · Emergency Lighting > FOUND DURING PREFLIGHT, FLIGHT DECK EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED EMEREGNCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKED SYSTEM GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA0052](https://openairdocs.org/sdr/GAIA0052.md): Light · inoperative · Feb 7, 2000 · N79748 · Boeing 727224 · Emergency Lighting > FLT 1849 - MSP-SEA - ENCOUNTERED DURING CRUISE, THE EMERGENCY EXIT LIGHTS REMAINED DIMLY ILLUMINATED. TURNED SWITCH ON AND LIGHTS ALL ILLUMINATED BRIGHTLY, BUT COULD NOT TURN OFF. THE FILGHT CONTINUED TO SEA AND LANDED SAFELY WITHOUT ANY FURTHER DIFFICULTIES - [SDR GAIA0043](https://openairdocs.org/sdr/GAIA0043.md): Light · unsecure · Jan 28, 2000 · N79748 · Boeing 727224 · Emergency Lighting > DURING ROUTINE MAINTENANCE AT TYS,THE COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY WAS FOUND UNSECURED. REINSTALLED COCKPIT EMERGENCY LIGHT ASSEMBLY. OPERATIONALLY CHECKED NORMAL. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA0042](https://openairdocs.org/sdr/GAIA0042.md): Bulb · failed · Jan 27, 2000 · N79748 · Boeing 727224 · Emergency Lighting > FOUND DURING ROUTINE MAINTENANCE AT MIA, THE LIGHT BULB INOPERATIVE FOR THE MAIN CABIN DOOR EMERGENCY EXIT LIGHT. REMOVED AND REPLACED BULB AT THE MAIN CABIN DOOR EMERGENCY EXIT LIGHT. OPERATIONALLY CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M) - [SDR GAIA0020](https://openairdocs.org/sdr/GAIA0020.md): Stringer · damaged · Jan 18, 2000 · N79748 · Boeing 727224 · Fuselage Main, Longeron/Stringer > FOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, DAMAGE WAS FOUND ON STRINGER 28R FROM BODY STATION 682 TO STATION 694. INSTALLED STRINGER REPAIR FROM STATION 682 TO STATION 694, - [SDR GAIA0021](https://openairdocs.org/sdr/GAIA0021.md): Skin · damaged · Jan 18, 2000 · N79748 · Boeing 727224 · Fuselage Main, Plate/Skin > FOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, DAMAGE WAS FOUND ALONG FUSELAGE SKIN FROM STATION 697 TO 708, BETWEEN STRINGER 28L AND STRINGER 28R. INSTALLED EXTERNAL DOUBLER REPAIR FROM STATION 697 TO STATION 708, BETWEEN STRING - [SDR GAIA0022](https://openairdocs.org/sdr/GAIA0022.md): Skin · damaged · Jan 18, 2000 · N79748 · Boeing 727224 · Fuselage Main, Plate/Skin > FOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, DAMAGE WAS FOUND ON EXTERIOR SKIN FROM STATION 575 TO 588 STRINGER 26L TO 27L. INSTALLED EXTERIOR FUSELAGE SKIN REPAIR FROM STATION 575 TO 588, STRINGER 26L TO 27L. MATERIAL USED 20 - [SDR GAIA0023](https://openairdocs.org/sdr/GAIA0023.md): Stringer · damaged · Jan 18, 2000 · N79748 · Boeing 727224 · Fuselage Main, Longeron/Stringer > FOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, DAMAGE WAS FOUND ALONG STRINGER AT STRINGER 27L FROM STATION 573 TO 588. INSTALLED STRINGER REPAIR AT STRINGER 27L FROM STATION 573 TO STATION 588. MATERIAL USED, PART NR BAC1498-14 - [SDR GAIA0024](https://openairdocs.org/sdr/GAIA0024.md): Floorbeam · damaged · Jan 18, 2000 · N79748 · Boeing 727224 · Fuselage Main, Floor Beam > FOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, DAMAGE WAS FOUND ON FLOORBEAM UPPER T CHORD AT STATION 344 FROM LBL 62.62 TO RBL 62.62. INSTALLED FLOORBEAM UPPER T CHORD REPAIR AT STATION 344 FROM LBL 62.62 TO RBL 62.62. MATERIAL - [SDR CALA9901293](https://openairdocs.org/sdr/CALA9901293.md): Panel · cracked · Sep 27, 1999 · N79748 · Boeing 727224 · Vertical Stabilizer, Plate/Skin > INSPECTION FOUND TWO 3 CRACKS IN VERTICAL STABILIZER SADDLE PANEL. THE SADDLE PANEL WAS REMOVED, REPAIRED IAW SRM 55-30-7, FIGURE3, AND REINSTALLED IAW MM 55-30-1, PAGE 201. - [SDR CALA9901291](https://openairdocs.org/sdr/CALA9901291.md): Skin · corroded · Sep 25, 1999 · N79748 · Boeing 727224 · Leading Edge Devices > INSPECTION FOUND NR 5 L/E FLAP BULL NOSE CORRODED. THE FLAP BULL NOSE WAS REMOVED AND REPLACED IAW MM 27-81-1, PAGE 401. - [SDR CALA9901287](https://openairdocs.org/sdr/CALA9901287.md): Skin · cracked · Sep 25, 1999 · N79748 · Boeing 727224 · Spoilers > INSPECTION FOUND A 2 INCH CRACK IN LT WING NR 7 SPOILER PANEL SKIN WITH DENTS ON LOWER SURFACE. THE SPOILER PANEL WAS REMOVED, REPAIRED, AND REINSTALLED IAW SRM 57-30-00, PAGE 30 AND MM 27-62-1, PAGE 403. - [SDR CALA9901290](https://openairdocs.org/sdr/CALA9901290.md): Fitting · cracked · Sep 24, 1999 · N79748 · Boeing 727224 · Wing, Landing Gear Attach Fittings > INSPECTION FOUND A 1.5 CRACK IN RT MLG BEAM SUPPORT FITTING. THE SUPPORT FITTING AND BUSHING WERE REMOVED AND REPLACED IAW ECRA 5740-01102. - [SDR CALA9901289](https://openairdocs.org/sdr/CALA9901289.md): Skin · debonded · Sep 24, 1999 · N79748 · Boeing 727224 · Spoilers > INSPECTION FOUND LT WING NR 2 SPOILER UPPER SKIN DEBONDED WITH SURFACE CORROSION AROUND SCREW HEADS. THE NR 2 SPOILER PANEL WAS REMOVED AND REPLACED IAW MM 27-61-1, PAGE 407. - [SDR CALA9901288](https://openairdocs.org/sdr/CALA9901288.md): Battery Pack · discharged · Sep 24, 1999 · N79748 · Boeing 727224 · Emergency Lighting > INSPECTION FOUND CABIN EMERGENCY AISLE PATH LIGHTING INOPERATIVE. MAINTENANCE FOUND A BLOWN FUSE AND INOPERATIVE BATTERY. THE FUSE AND BATTERY PACK WERE REMOVED AND REPLACED IAW MM 33-50-1. - [SDR CALA9901270](https://openairdocs.org/sdr/CALA9901270.md): Fitting · corroded · Sep 20, 1999 · N79748 · Boeing 727224 · Wing Miscellaneous Structure > INSPECTION FOUND RT MLG BEAM H FITTING ATTACH HOLE AND UPPER FORWARD LUG CORRODED. THE ATTACH HOLE WAS REPAIRED IAW ECRA 5740-01903, PAGE 2 AND THE FITTING WAS REPLACED. - [SDR CALA9901269](https://openairdocs.org/sdr/CALA9901269.md): Fitting · cracked · Sep 20, 1999 · N79748 · Boeing 727224 · Wing Miscellaneous Structure > INSPECTION FOUND A.75 INCH CRACK IN RT WING REAR SPAR O/B ATTACH FITTING FOR MLG. THE FITTING WAS REMOVED AND REPLACED IAW ECRA 5740-01901. - [SDR CALA9901268](https://openairdocs.org/sdr/CALA9901268.md): Track · corroded · Sep 20, 1999 · N79748 · Boeing 727224 · Trailing Edge Flaps > INSPECTION FOUND RT WING NR 5 FLAP TRACK CORRODED. THE FLAP TRACK WAS REMOVED AND REPLACED IAW MM 27-51-31, PAGE 402-410. - [SDR CALA9901130](https://openairdocs.org/sdr/CALA9901130.md): Casting · cracked · Sep 5, 1999 · N79748 · Boeing 727224 · Emergency Exits > INSPECTION FOUND A 1 INCH CRACK IN RT FORWARD OVERWING DOOR INNER UPPER CASTING. THE CASTING WAS REMOVED AND A NEW CASTING WAS INSTALLED IAW SRM 51-30-2, FIGURE 1. - [SDR CALA9901103](https://openairdocs.org/sdr/CALA9901103.md): Battery Pack · discharged · Aug 30, 1999 · N79748 · Boeing 727224 · Emergency Lighting > INSPECTION FOUND FORWARD OVERHEAD EMERGENCY LIGHT AT ROW NR 2 INOPERATIVE. MAINTENANCE FOUND THE BATTERY PACK AT FAULT. THE BATTERY PACK WAS RECHARGED AND REINSTALLED. OPERATION CHECKED GOOD IAW MM 33-50-81, PAGE 403. - [SDR CALA9901102](https://openairdocs.org/sdr/CALA9901102.md): Fitting · corroded · Aug 30, 1999 · N79748 · Boeing 727224 · Trailing Edge Flaps > INSPECTION FOUND FORWARD END OF LT WING NR 4 FLAP TRACK FITTING CORRODED. THE FITTING WAS REMOVED AND REPLACED. THE FLAP TRACK WAS REINSTALLED IAW MM 27-51-72, PAGE 401. Next page: https://openairdocs.org/deregistered/N79748-2011-05-04/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 = 'N79748' AND deregistration_id = 'N79748-2011-05-04' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N79748-2011-05-04/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.