# Service difficulty reports: N77780, cancelled Apr 29, 2013

A list on [N77780, cancelled Apr 29, 2013](https://openairdocs.org/deregistered/N77780-2013-04-29.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 · 103 reports

- [SDR GAIA02108OP](https://openairdocs.org/sdr/GAIA02108OP.md): Clamp · loose · Sep 19, 2002 · N77780 · Boeing 727232 · Pneumatic Distribution System
  > FLT 778 - FWA-BOS - DURING CRUISE, THE NR 1 ENGINE STRUT LIGHT ILLUMINATED. ACCOMPLISHED AOM PROCEDURE AND THE LIGHT EXTINGUISHED. THE AIRCRAFT CONTINUED TO BOS AND LANDED WITHOUT FURTHER OCCURRENCE. FOUND A LOOSE CLAMP AT THE SIXTH STAGE CHECK VALVE IN THE
- [SDR GAIA02069OP](https://openairdocs.org/sdr/GAIA02069OP.md): Accessory Unit · failed · Jun 7, 2002 · N77780 · Boeing 727232 · Landing Gear Retraction/Extension System
  > DURING APPROACH OF FLIGHT NR 1849 FROM MSP TO SEA, THE RIGHT MAIN LANDING GEAR INDICATED UNSAFE. CREW DID A 'GO AROUND' AND ON SECOND APPROACH GOT ALL GREEN LIGHTS. SECONDARY INDICATIONS WERE NORMAL. CREW DECLARED AN EMERGENCY INTO SEA. AIRCRAFT LANDED WIT
- [SDR GAIA02016ST](https://openairdocs.org/sdr/GAIA02016ST.md): Stringer · corroded · Feb 6, 2002 · N77780 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > DURING A CPCP INSPECTION DISCOVERED FORWARD CARGO COMPARTMENT STATION 540 STRINGER 23R CORROSION ON STRINGER. ACCOMPLISHED STRINGER REPAIR AT BS 540 STRINGER 23R IAW B727 SRM 53-10-3 FIG 1. (M)
- [SDR GAIA02015ST](https://openairdocs.org/sdr/GAIA02015ST.md): Shear Tie · corroded · Feb 6, 2002 · N77780 · Boeing 727232 · Fuselage Main, Structure
  > DURING A CPCP INSPECTION DISCOVERED C3 DOOR AFT FRAME BS 1148 SHEAR TIE ABOVE STRINGER 23R IS CORRODED. ACCOMPLISHED BS 1148 SHEAR TIE REPLACEMENT ABOVE STRINGER 23R IAW B727 SRM 53-10-2 FIG 5. (M)
- [SDR GAIA02014ST](https://openairdocs.org/sdr/GAIA02014ST.md): Keelbeam · cracked · Feb 6, 2002 · N77780 · Boeing 727232 · Fuselage Main, Keel
  > DURING A CPCP INSPECTION DISCOVERED RIGHT WHEEL WELL BS 870 AND KEEL BEAM FRAME ANGLE IS CRACKED, 1 INCH LONG APPROX. ACCOMPLISHED BS 870 AND KEEL BEAM FRAME ANGLE REPLACEMENT IN THE RIGHT WHEEL WELL IAW B727 SRM 51-30-2. (M)
- [SDR GAIA02013ST](https://openairdocs.org/sdr/GAIA02013ST.md): Keelbeam · cracked · Feb 6, 2002 · N77780 · Boeing 727232 · Fuselage Main, Keel
  > DURING A CPCP INSPECTION DISCOVERED LEFT WHEEL WELL BS 870 KEEL BEAM WEB SHOWS CRACK JUST FORWARD OF APU CUT OUT, 3 INCH LONG APPROX. ACCOMPLISHED BS 870 KEEL BEAM WEB REPAIR IN THE LEFT WHEEL WELL IAW B727 SRM 51-40-2 FIG 1. (M)
- [SDR GAIA02012ST](https://openairdocs.org/sdr/GAIA02012ST.md): Frame · cracked · Feb 6, 2002 · N77780 · Boeing 727232 · Fuselage Main, Frame
  > DURING A CPCP INSPECTION DISCOVERED RIGHT WHEEL WELL TOP OUTBOARD BS 910 FRAME SHOWS CRACK TO BOTTOM INSIDE, 3 INCHES LONG APPROX. ACCOMPLISHED BS 910 FRAME REPAIR IN THE RIGHT WHEEL WELL IAW WITH B727 SRM 51-40-3 FIG 1. (M)
- [SDR GAIA01001](https://openairdocs.org/sdr/GAIA01001.md): Light · inoperative · Jan 3, 2001 · N77780 · Boeing 727232 · Emergency Lighting
  > BOS - MAIN ENTRY EMERGENCY EXIT LIGHT WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. OPS CHECK GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00718](https://openairdocs.org/sdr/GAIA00718.md): Actuator · inoperative · Nov 22, 2000 · N77780 · Boeing 727232 · Leading Edge Slat Actuator
  > FLT 3736 - BNA-FWA - NR 5 LEADING EDGE FLAP DID NOT FULLY EXTEND ON FLAP EXTENSION. HOWEVER, AT SLOW SPEED, FLAP FULLY EXTENDED. AIRCRAFT MADE AN UNEVENTFUL LANDING AT FWA. REMOVED AND REPLACED NR 5 KRUEGER FLAP ACTUATOR IAW 272 MM 27-81-22. OPS CHECK GOOD
- [SDR GAIA00690](https://openairdocs.org/sdr/GAIA00690.md): Actuator · inoperative · Nov 10, 2000 · N77780 · Boeing 727232 · Leading Edge Slat Actuator
  > BNA/FWA - FLT 3735 - DURING LANDING, THE NR 5 LE KRUGER FLAP DID NOT FULLY EXTEND ON FLAP EXTENSION. THE CREW DECLARED AN EMERGENCY. AIRCRAFT LANDED SAFELY. MAINTENANCE REMOVED AND REPLACED THE NR 5 LE KRUGER FLAP ACTUATOR. OPS CHECK PERFORMED, AIRCRAFT RE
- [SDR GAIA00511](https://openairdocs.org/sdr/GAIA00511.md): Battery · inoperative · Sep 5, 2000 · N77780 · Boeing 727232 · Emergency Lighting
  > DFW MAINTENANCE FOUND MAIN ENTRY EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REINSTALLED SERVICEABLE BATTERIES. OPS CHECK GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00510](https://openairdocs.org/sdr/GAIA00510.md): Light · inoperative · Sep 5, 2000 · N77780 · Boeing 727232 · Emergency Lighting
  > DFW MAINTENANCE FOUND COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REINSTALLED SERVICEABLE EMERGENCY LIGHT ASSEMBLY. OPS CHECK GOOD ON GROUND. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00368](https://openairdocs.org/sdr/GAIA00368.md): Battery · discharged · Jun 22, 2000 · N77780 · Boeing 727232 · Emergency Lighting
  > CLT - EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REINSTALLED SERVICEABLE BATTERY FOR L-1 AND COCKPIT EMERGENCY LIGHT UNITS. OPS CHECK GOOD ON GROUND. RECYCLED BATTERY CHARGER SYSTEM. AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA00283](https://openairdocs.org/sdr/GAIA00283.md): Wire · chafed · May 24, 2000 · N77780 · Boeing 727232 · Landing Gear System Wiring
  > FLT 1759 - MEM-FWA - RIGHT MAIN GEAR, RED UNSAFE LIGHT AND GREEN LIGHT ILLUMINATED DURING FLIGHT. AIRCRAFT LANDED IN FWA WITH NO FURTHER DIFFICULTIES. FOUND INSULATION CHAFED ON UPLOCK PROXIMITY SWITCH FOR RIGHT MAIN LANDING GEAR. REPAIRED WIRE AND SECURED
- [SDR GAIA00277](https://openairdocs.org/sdr/GAIA00277.md): Connector · dirty · May 14, 2000 · N77780 · Boeing 727232 · Leading Edge Slat Position Indicating System
  > MEM/IAH - FLT 1760 - AFTER FLAP RETRACTION, NR 4 LEADING EDGE DEVICE DID NOT INDICATE RETRACTED. PERFORMED ABNORMAL PROCEDURE WITH THE SAME RESULTS. THE CREW RETURNED TO MEM AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. CLEANED CONNECTOR AT SWITCH AND OPERAT
- [SDR GAIA00117](https://openairdocs.org/sdr/GAIA00117.md): Indicator · malfunctioned · Mar 23, 2000 · N77780 · Boeing 727232 · Landing Gear Position and Warning
  > FLT 2030 - MHR-PDX - AFTER TAKEOFF, RIGHT MAIN GEAR FAILED TO INDICATE UP AND LOCKED. AFTER THREE MINUTES, WITH GEAR UP, LIGHTS EXTINGUISHED. PERFORMED FLY-BY BY TOWER, AND GEAR WAS VISUALLY CHECK UP. OPERATIONALLY CHECKED NORMAL DURING GEAR EXTENSION FOR A
- [SDR GAIA0054](https://openairdocs.org/sdr/GAIA0054.md): Connector · dirty · Feb 11, 2000 · N77780 · Boeing 727232 · Landing Gear Position and Warning
  > FLT 2507 - PDX - RIGHT GEAR LIGHT ON DURING TAKEOFF ROLL. CLEANED CANNON PLUG. FUNCTIONAL TEST GOOD. LIGHT STAYED GREEN AIRCRAFT RETURNED TO SERVICE. (M)
- [SDR GAIA99227](https://openairdocs.org/sdr/GAIA99227.md): Bulkhead · cracked · Dec 1, 1999 · N77780 · Boeing 727232 · Fuselage Main, Bulkhead
  > FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. TAIL SKID CAVITY BULKHEAD WEB AT STATION 1183 HAS CRACK ON LEFT SIDE 5 INCHES BELOW FLOOR. REMOVED EXISTING REPAIR AND INSPECTE
- [SDR GAIA99226](https://openairdocs.org/sdr/GAIA99226.md): Floorbeam · cracked · Dec 1, 1999 · N77780 · Boeing 727232 · Fuselage Main, Floor Beam
  > FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEABY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, BS 1183 BULKHEAD LEFT VERTICAL BEAM HAS CRACK AT LOWER END, LBL 8. PERFORMED NDT INSPECTION TO DETERMINE END OF CRACK, PER B727
- [SDR GAIA99225](https://openairdocs.org/sdr/GAIA99225.md): Frame · corroded · Dec 1, 1999 · N77780 · Boeing 727232 · Fuselage Main, Frame
  > FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. NOSE SECTION INTERNAL CIRCUMFERENTIAL FRAME HAS CORROSION ON LEFT SIDE OF DOG HOUSE BELOW HORIZONTAL WALKWAY BEAM BS 303 AND STR
- [SDR GAIA99224](https://openairdocs.org/sdr/GAIA99224.md): Vent Lines · chafed · Dec 1, 1999 · N77780 · Boeing 727232 · Fuel Storage
  > FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. FUEL VENT TUBING WAS FOUND TO BE CHAFING AT THE FOLLOWING WING STATIONS, LWS 656.5, LWS 546.5, LWS 519.0, RWS 601.5 AND RWS 546
- [SDR GAIA99223](https://openairdocs.org/sdr/GAIA99223.md): Angle · cracked · Dec 1, 1999 · N77780 · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. MAIN CABIN STRINGER 17L BODY STATION 850, ANGLE IS CRACKED, INBOARD SIDE OF FRAME. ACCOMPLISHED REPAIR ON MAIN CABIN STRINGER
- [SDR GAIA99222](https://openairdocs.org/sdr/GAIA99222.md): Stringer · corroded · Dec 1, 1999 · N77780 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY (MIAMI) PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. CORROSION AT STRINGER 7R UPPER FLANGE, JUST FORWARD OF BS 1148. REMOVED CORRODED AREA AT STRINGER 7R UPPER FLANGE FORWA
- [SDR GAIA99221](https://openairdocs.org/sdr/GAIA99221.md): Seat Track · mismanufactured · Dec 1, 1999 · N77780 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND DURING 'ZERO B, TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. SEAT TRACK AT LBL 24.75 TOO SHORT AT SPLICES FOR CARGO MOD BODY STATION 1050 TO 1070. REMOVED AND REPLACED SEAT TRACK AT LBL 2
- [SDR GAIA99220](https://openairdocs.org/sdr/GAIA99220.md): Bear Strap · cracked · Dec 1, 1999 · N77780 · Boeing 727232 · Fuselage Main, Plate/Skin
  > FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE. FORWARD GALLEY DOOR CUTOUT AT LOWER AFT CORNER BEAR STRAP HAS CRACK. STOP DRILLED CRACK AT GALLEY DOOR CUTOUT BEAR STRAP IAW B7
- [SDR GAIA99219](https://openairdocs.org/sdr/GAIA99219.md): Floorbeam · corroded · Dec 1, 1999 · N77780 · Boeing 727232 · Fuselage Main, Floor Beam
  > FOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, CABIN FORWARD GALLEY FLOORBEAM AT BODY STATION 380, RBL 14 TO RBL 64 IS CORRODED. REMOVED CORROSION AT FLOORBEAM. CUTOUT AND REM
- [SDR GAIA99218](https://openairdocs.org/sdr/GAIA99218.md): Seat Track · mismanufactured · Dec 1, 1999 · N77780 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND DURING ZERO B TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, SEAT TRACK AT RBL 45.5 IS TOO SHORT FOR CARGO MOD AT SPLICE, BODY STATION 1090 TO 1110. REMOVED AND REPLACED SEAT TRACK AT RBL 45.
- [SDR GAIA99217](https://openairdocs.org/sdr/GAIA99217.md): Seat Track · mismanufactured · Dec 1, 1999 · N77780 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND DURING ZERO B TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, SEAT TRACK AT LBL 45.5 TOO SHORT FOR CARGO MOD BODY STATION 1110 TO 1130. REMOVED AND REPLACED SEAT TRACK AT LBL 45.5 FROM BS 1030
- [SDR GAIA99216](https://openairdocs.org/sdr/GAIA99216.md): Floorbeam · corroded · Dec 1, 1999 · N77780 · Boeing 727232 · Fuselage Main, Floor Beam
  > FOUND DURING ZERO B, TRANSITION CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, CABIN FLOORBEAM AT BODY STATION 400, RBL 12 CORRODED. REMOVED CORROSION AT FLOORBEAM. CUTOUT AND REMOVED DAMAGED AREAS PER SRM 5
- [SDR GAIA99215](https://openairdocs.org/sdr/GAIA99215.md): Seat Track · mismanufactured · Dec 1, 1999 · N77780 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KGA CERTIFICATE, SEAT TRACK AT RBL 45.5, BS 680 TO BS 720A HAS WRONG SPLICE FOR 9G BULKHEAD. REMOVED AND REPLACED SEAT TRACK AT RBL 45.5 FROM STA
- [SDR GAIA99214](https://openairdocs.org/sdr/GAIA99214.md): Seat Track · mismanufactured · Dec 1, 1999 · N77780 · Boeing 727232 · Fuselage, Seat/Cargo Attach Fittings
  > FOUND DURING 'ZERO B TRANSITION' CHECK AT AVBORNE HEAVY MAINTENANCE FACILITY, PRIOR TO THIS AIRCRAFT BEING ON THE KHA CERTIFICATE, SEAT TRACK AT RBL 24.75 TOO SHORT FOR CARGO MOD BODY STATION 1090 TO 1110. REMOVED AND REPLACED SEAT TRACK AT RBL 24.75 FROM BS
- [SDR CALA9900305](https://openairdocs.org/sdr/CALA9900305.md): Skin · dented · Mar 22, 1999 · N77780 · Boeing 727232 · Spoilers
  > INSPECTION FOUND RT WING NR 9 SPOILER DENTED ON LOWER END. THE NR 9 SPOILER WAS REMOVED AND REPLACED IAW MM 27-62-1.
- [SDR CALA9900304](https://openairdocs.org/sdr/CALA9900304.md): Light · inoperative · Mar 22, 1999 · N77780 · Boeing 727232 · Emergency Lighting
  > INSPECTION FOUND AFT ENTRY OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. THE LIGHT ASSEMBLY WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-50-00.
- [SDR CALA9900303](https://openairdocs.org/sdr/CALA9900303.md): Panel · bent · Mar 22, 1999 · N77780 · Boeing 727232 · Spoilers
  > INSPECTION FOUND RT WING NR 8 SPOILER OUTBOARD AREA BENT UP. THE SPOILER PANEL WAS REMOVED AND REPLACED IAW MM 27-62-1.
- [SDR CALA9900296](https://openairdocs.org/sdr/CALA9900296.md): Stiffener · corroded · Mar 18, 1999 · N77780 · Boeing 727232 · Wing Miscellaneous Structure
  > INSPECTION FOUND STIFFENER CORRODED AT RT WING FRONT SPAR FS 249. THE CORRODED SECTION OF STIFFENER WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 51-30-02, PAGE 4.
- [SDR CALA9900295](https://openairdocs.org/sdr/CALA9900295.md): Stringer · corroded · Mar 18, 1999 · N77780 · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND STRINGER 28R CORRODED AT BS 1164. THE CORRODED SECTION OF STRINGER WAS REMOVED AND A NEW SECTION OF STRINGER WAS INSTALLED IAW SRM 51-30-2 AND 51-10-2.
- [SDR CALA9900294](https://openairdocs.org/sdr/CALA9900294.md): Bolts · corroded · Mar 18, 1999 · N77780 · Boeing 727232 · Vertical Stabilizer
  > INSPECTION FOUND VERTICAL STABILIZER TENSION TIE BOLTS (8) PITTED AND CORRODED. THE TENSION TIE BOLTS WERE REMOVED AND REPLACED IAW MM 55-30-51, PAGE 406-408.
- [SDR CALA9900293](https://openairdocs.org/sdr/CALA9900293.md): Intercostal · corroded · Mar 18, 1999 · N77780 · Boeing 727232 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LOWER FLANGE OF INTERCOSTAL CORRODED IN AFT CARGO AREA AT STA 1128-1148 OUTBOARD OF STRINGER 28R. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-10-2.
- [SDR CALA9900292](https://openairdocs.org/sdr/CALA9900292.md): Bracket · cracked · Mar 18, 1999 · N77780 · Boeing 727232 · Leading Edge Slat Actuator
  > INSPECTION FOUND A 1 INCH CRACK IN INBOARD SUPPORT BRACKET AT TOP AND BOTTOM OF NR 6 LEADING EDGE FLAP ACTUATOR. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2.
- [SDR CALA9900291](https://openairdocs.org/sdr/CALA9900291.md): Cowl · cracked · Mar 18, 1999 · N77780 · Boeing 727232 · Engine Cowling System
  > INSPECTION FOUND A 2 INCH CRACK IN NR 3 ENGINE NOSE COWL ACOUSTIC LINING WITH LINING ERODED IN SEVERAL AREAS. THE NR 3 ENGINE NOSE COWL WAS REMOVED AND REPLACED IAW MM 54-00.
- [SDR CALA9900290](https://openairdocs.org/sdr/CALA9900290.md): Housing · corroded · Mar 18, 1999 · N77780 · Boeing 727232 · Horizontal Stabilizer Structure
  > INSPECTION FOUND HORIZONTAL STABILER LEFT AND RIGHT HINGE BUSHING HOUSINGS CORRODED. THE BUSHINGS AND BEARINGS WERE REMOVED AND REPLACED IAW ECRA 555C028 AND ECRA 5550-01033.
- [SDR CALA9900289](https://openairdocs.org/sdr/CALA9900289.md): Bolt · corroded · Mar 18, 1999 · N77780 · Boeing 727232 · Horizontal Stabilizer Structure
  > INSPECTION FOUND BOTH HORIZONTAL STABILIZER HINGE PIN BOLTS CORRODED. BOTH HINGE PINS WERE REPLACED IAW MM 55-00.
- [SDR CALA9900288](https://openairdocs.org/sdr/CALA9900288.md): Wire · broken · Mar 18, 1999 · N77780 · Boeing 727232 · Light System Wiring
  > INSPECTION FOUND EXIT IDENTIFIER LIGHT AT R-2 DOOR INOPERATIVE. MAINTENANCE FOUND EXIT LIGHT WIRE BROKEN. THE WIRE WAS REPAIRED IAW MM 33-51-00, PAGE 903 AND OPERATION WAS RESTORED.
- [SDR CALA9900287](https://openairdocs.org/sdr/CALA9900287.md): Wire · broken · Mar 18, 1999 · N77780 · Boeing 727232 · Light System Wiring
  > INSPECTION FOUND THE EXIT IDENTIFIER LIGHT AT L-2 DOOR INOPERATIVE. MAINTENANCE FOUND A BROKEN GROUND WIRE. THE WIRE WAS REPAIRED IAW MM 33-51-00, PAGE 903 AND OPERATION WAS RESTORED.
- [SDR CALA9900286](https://openairdocs.org/sdr/CALA9900286.md): Wire · loose · Mar 18, 1999 · N77780 · Boeing 727232 · Light System Wiring
  > INSPECTION FOUND EXIT IDENTIFIER LIGHT AT LEFT AFT LAV WALL INOPERATIVE. MAINTENANCE FOUND A LOOSE GROUND WIRE. THE WIRE WAS SECURED IAW MM 33-51-00, PAGE 903 AND OPERATION WAS RESTORED.
- [SDR CALA9900285](https://openairdocs.org/sdr/CALA9900285.md): Skin · cracked · Mar 18, 1999 · N77780 · Boeing 727232 · Elevator, Spar/Rib
  > INSPECTION FOUND A 1 INCH CRACK IN LEFT ELEVATOR LOWER SKIN JUST I/B AND AFT OF PANEL NR 9311. THE CRACK WAS STOP DRILLED IAW SRM 55-20-3. A DOUBLER WAS INSTALLED IAW SRM 55-20-3, 51-10-2, AND 51-30. A CALCULATED BALANCE WAS PERFORMED IAW SRM 51-80-7 AND WA
- [SDR CALA9900284](https://openairdocs.org/sdr/CALA9900284.md): Skin · cracked · Mar 18, 1999 · N77780 · Boeing 727232 · Leading Edge Devices
  > INSPECTION FOUND TWO.5 INCH CRACKS COMING FROM SCREW HOLE TO RIVETS AT RT WING NR 7 SLAT UPPER TRAILING EDGE WHERE O/B HOOK MOUNTS. REMOVED FASTENERS IAW SRM 51-30-2. A REPAIR DOUBLER WAS INSTALLED IAW SRM 57-20-3.
- [SDR CALA9900283](https://openairdocs.org/sdr/CALA9900283.md): Skin · cracked · Mar 18, 1999 · N77780 · Boeing 727232 · Spoilers
  > INSPECTION FOUND A.1875 INCH CRACK AT RT WING UPPER TRAILING EDGE AT CUTOUT FOR NR 13 SPOILER SECOND FROM O/B HINGE CUTOUT. THE CRACK WAS STOP DRILLED. A REPAIR WAS INSTALLED AND EDGES WERE SEALED IAW SRM 51-10-1 AND 51-10-3, PAGE 4.
- [SDR CALA9900282](https://openairdocs.org/sdr/CALA9900282.md): Angle · cracked · Mar 17, 1999 · N77780 · Boeing 727232 · Leading Edge Devices
  > INSPECTION FOUND A.125 INCH CRACK IN RT WING NR 7 SLAT LOWER SPANWISE CHORD ANGLE AT CUTOUT FOR I/B TRACK AND A.3125 INCH CRACK AT STOP PAD AREA SIX INCHES INBOARD. THE ANGLE WAS REMOVED. AN ANGLE AND REPAIR SPLICE WERE INSTALLED IAW SRM 51-40-3, 51-10-2,
- [SDR CALA9900281](https://openairdocs.org/sdr/CALA9900281.md): Skin · cracked · Mar 17, 1999 · N77780 · Boeing 727232 · Trailing Edge Flaps
  > INSPECTION FOUND A 1.25 INCH CRACK IN RT O/B FOREFLAP LEADING EDGE. THE CRACK WAS STOP DRILLED. A DOUBLER WAS INSTALLED IAW SRM 57-50-4 AND 51-30-2, PAGE 7.

Next page: https://openairdocs.org/deregistered/N77780-2013-04-29/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 = 'N77780' AND deregistration_id = 'N77780-2013-04-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N77780-2013-04-29/reports

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