# Service difficulty reports: Boeing 727-260

A list on [Boeing 727-260](https://openairdocs.org/model/boeing-727-260.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 70 reports

- [SDR CA150506005](https://openairdocs.org/sdr/CA150506005.md): Roller Cam · sheared · May 5, 2015 · Boeing 727260 · Passenger/Crew Doors
  > (CAN) DURING DAILY MAINTENANCE, THE AFT LOWER ROLLER CAM ON THE MAIN ENTRANCE DOOR WAS FOUND SHEARED OFF. THE ROLLER CAM WAS REPLACED IAW THE AMM AND FUNCTION CHECKED SERVICEABLE. THE ACFT WAS RETURNED TO SERVICE.
- [SDR CA150505008](https://openairdocs.org/sdr/CA150505008.md): Roller Cam · sheared · Apr 21, 2015 · Boeing 727260 · Passenger/Crew Doors
  > (CAN) WHILE CLOSING MAIN ENTRANCE DOOR, THE UPPER AFT CRANK ROLLER CAM SHAFT SHEARED. THE SHEARED CRANK ROLLER CAM WAS REPLACED AND CHECKED IAW THE AMM. THE ACFT WAS RETURNED TO SERVICE.
- [SDR CA150224030](https://openairdocs.org/sdr/CA150224030.md): Mount · misaligned · Feb 23, 2015 · Boeing 727260 · Engine Mount Section
  > (CAN) DURING ROUTINE MAINTENANCE INSPECTION THE NR 2 ENGINE RT FORWARD ISOLATOR MOUNT ALIGNMENT MARKS WERE FOUND MISALIGNED AND BONDING STRAP SHEARED.
- [SDR CA120817009](https://openairdocs.org/sdr/CA120817009.md): Sliding Window · cracked · Jul 31, 2012 · Boeing 727260 · Flight Compartment Windows
  > (CAN) R2 WINDOW OUTER PANE FAILED IN CRUISE, ACFT LANDED WITHOUT INCIDENT MAINTENANCE REPLACED WINDOW ASSY.
- [SDR CA120112007](https://openairdocs.org/sdr/CA120112007.md): Duct · cracked · Jan 4, 2012 · Boeing 727260 · Engine Anti-Icing System
  > (CAN) ON DECENT CREW OBSERVED NR 2 ENGINE FIRE WARNING INDICATION. COMPLETED FIRE DRILL, FIRE LIGHT STAYED ON, FIRE BOTTLE DISCHARGED. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE IGV ANTI-ICE DUCT CRACKED AT WELDED FLANGE. DUCT AND FI
- [SDR CA111212015](https://openairdocs.org/sdr/CA111212015.md): Module · bypassing · Dec 8, 2011 · Boeing 727260 · Rudder Control System
  > (CAN) DURING TAXI WHEN FLAPS EXTENDED HYD A SYS PRESS WENT TO 1500 PSI & BOTH A SYS LOW PRESS LIGHTS CAME ON. UPON REMOVAL OF RUDDER MODULE FOUND TEFLON BACK UP RING OUT OF PLACE & WOUND UP INSIDE THE LINE FITTING PORT. REPAIR VENDOR REQUESTED TO SEND STRIP
- [SDR CA091022004](https://openairdocs.org/sdr/CA091022004.md): Windshield · cracked · Oct 20, 2009 · Boeing 727260 · Flight Compartment Windows
  > (CAN) DURING CRUISE AT FL320, THE CAPTAINS L1 WINDOW OUTER PANE CRACKED. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT AND THE WINDOW WAS REPLACED BY MAINTENANCE PERSONNEL. WHEN COMPLETE THE AIRCRAFT WAS RETURNED TO SERVICE. (TC 20091022004)
- [SDR CA090526008](https://openairdocs.org/sdr/CA090526008.md): Actuator · corroded · Mar 3, 2009 · Boeing 727260 · Stabilizer Actuator
  > (CAN) UNIT REMOVED FOR SCHEDULED OVERHAUL. UPON DISASSEMBLY, INTERNAL COMPONENTS BADLY CORRODED AND CONTAMINATED WITH WATER. UNIT SCRAPPED. THERE WERE NO INFLIGHT DEFECTS REPORTED.
- [SDR CA080905003](https://openairdocs.org/sdr/CA080905003.md): Controller · malfunctioned · Sep 3, 2008 · Boeing 727260 · Compressor Bleed Control
  > (CAN) AT FL300, TOP OF DESCENT, AS THRUST REDUCTION COMMENCED, LARGE BANG WAS EXPERIENCED BY THE FLIGHT CREW WITH FLUCTUATIONS IN NR 2 ENGINE PARAMETERS. ENGINE WAS IDLED FOR THE REMAINDER OF THE FLIGHT AND SHUT DOWN UPON LANDING. MX PERSONNEL CARRIED OUT TRO
- [SDR CA080423004](https://openairdocs.org/sdr/CA080423004.md): Windscreen · burned · Apr 16, 2008 · Boeing 727260 · Flight Compartment Windows
  > (CAN) AFTER COCKPIT SETUP SMOKE AND FLAME WAS OBSERVED BY THE FLIGHT CREW FROM THE TOP LT CORNER OF THE R1 WINDOW. WHEN THE R1 WINDOW HEAT WAS SELECTED OFF THE FLAME AND SMOKE CEASED. THE R1 WINDSCREEN WINDOW HEAT SYS WAS DEFERRED BY MAINT. UPON ARRIVAL AT TH
- [SDR CA070911012](https://openairdocs.org/sdr/CA070911012.md): Stud · dislodged · Sep 5, 2007 · Boeing 727260 · Turbine Engine Accessory Drive
  > (CAN) DURING CRUISE, THE NR 2 OIL QUANTITY SLOWLY DECREASED TO ZERO. WHEN THE OIL QUANTITY WENT BELOW THE GREEN ARC THE FLIGHT CREW SHUTDOWN THE ENGINE USING THE APPROPRIATE CHECKLIST AND AN EMERGENCY WAS DECLARED INTO AIRFIELD. THE AIRCRAFT LANDED WITHOUT FUR
- [SDR CA070531003](https://openairdocs.org/sdr/CA070531003.md): Pitot System · obstructed · May 30, 2007 · Boeing 727260 · Pitot/Static System
  > (CAN) THE AIRCRAFT BEGAN THE TAKEOFF ROLL WHEN THE FLIGHT CREW NOTICED A LAG IN THE FIRST OFFICERS AIR SPEED INDICATION. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WITH NO ADDITIONAL PROBLEMS. UPON INSPECTION OF THE FIRST OFFICERS PITOT INST
- [SDR CA070518005](https://openairdocs.org/sdr/CA070518005.md): Duct · ruptured · May 16, 2007 · Boeing 727260 · Engine Bleed Air System
  > (CAN) WHILE PERFORMING THE DAILY INSPECTION, MAINTENANCE PERSONNEL HEARD A LOUD BANG, WHICH WAS FOLLOWED BY A DROP IN APU DUCT PRESSURE TO 0 PSI. UPON INSPECTION, 2 BLEED AIR DUCTS WERE FOUND RUPTURED, FORWARD OF THE APU LOAD CONTROL VALVE THAT CONNECT TO THE
- [SDR CA050718008](https://openairdocs.org/sdr/CA050718008.md): Fire Loop · failed · Jul 12, 2005 · Boeing 727260 · Fire Detection
  > DURING CLIMB AT FL120, NR 3 ENGINE FIRE WARNING LIGHT ILLUMINATED AND ASSOCIATED WARNING HORN SOUNDED INTERMITTENTLY. CREW FOLLOWED ENGINE FIRE EMERGENCY CHECKLIST SECURED ENGINE AND FIRE EXTINGUISHER BOTTLES WERE ACTIVATED. ENGINE FIRE INDICATION REMAINED,
- [SDR CA050512004](https://openairdocs.org/sdr/CA050512004.md): Controller · failed · May 5, 2005 · Boeing 727260 · Cabin Pressure Controller
  > DURING DESCENT FROM FL290 TO FL270, THE 'OFF SCHEDULE' DESCENT LIGHT ILLUMINATED. CABIN ALTITUDE WAS QUICKLY INCREASING WITH CABIN DIFFERENTIAL QUICKLY DECREASING. CREW SWITCHED TO STANDBY, MANUAL DC AND MANUAL AC BUT CABIN CONTINUED TO DE-PRESSURIZE. ATC W
- [SDR CA050105003](https://openairdocs.org/sdr/CA050105003.md): Control System · failed · Dec 20, 2004 · Boeing 727260 · Leading Edge Slat Control System
  > (CAN) DURING CLIMB FLAPS/SLATS SELECTED UP. FLAPS INDICATED UP, SLAT AMBER REMAINED ON AND AIRCRAFT ROLLED TO THE RT. SECOND OFFICERS PANEL INDICATED NR6 SLAT STILL IN TRANSIT. FLAPS AND SLATS CYCLED A NUMBER OF TIMES TO NO AVAIL. DECISION TO RETURN WAS MADE,
- [SDR CA041214007](https://openairdocs.org/sdr/CA041214007.md): Indicator · unreliable · Dec 9, 2004 · Boeing 727260 · Engine Oil Quantity
  > (CAN) DURING CLIMB ENGINE NR 2 OIL QUANTITY DECREASED RAPIDLY TO ZERO, FOLLOWED BY A RISE IN OIL TEMP. CREW SHUTDOWN THE ENGINE ANDRETURNED TO AIRPORT. MAINTENANCE CHECKED OIL QTY AND FOUND TANK FULL. MAIN OIL FILTER CHECKED FOR CONTAMINATION, NONE FOUND. BEA
- [SDR CA040625006](https://openairdocs.org/sdr/CA040625006.md): Shutoff Valve · leaking · Jun 24, 2004 · Boeing 727260 · Engine Anti-Icing System
  > (CAN) DURING CLIMB NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. OPS CHECKLIST CARRIED OUT. AIRCRAFT WAS RETURNED TO BASE DUE TO SECOND INCIDENT IN 2 DAYS. DURING INSPECTION, NR 1 ANTI ICE VALVE SEALS WERE REPLACED. NR 1 BLEED SHUT OFF VALVE WAS REPLACED IAW
- [SDR CA040625002](https://openairdocs.org/sdr/CA040625002.md): Fire Loop · malfunctioned · Jun 24, 2004 · Boeing 727260 · Fire Detection
  > (CAN) DURING FLIGHT, NR 3 ENGINE FIRE WARNING INDICATION WAS ACTIVATED. BELL WAS INTERMITTENT BUT BECAME A LITTLE MORE STEADY. EMERGENCY PROCEDURES WERE INITIATED AND NR 3 ENGINE WAS SHUTDOWN. FIRE HANDLE WAS PULLED BUT NOT TO RELEASE EXTINGUISHING AGENT.
- [SDR CA040625005](https://openairdocs.org/sdr/CA040625005.md): Modulating Valve · leaking · Jun 22, 2004 · Boeing 727260 · Engine Anti-Icing System
  > (CAN) DURING CLIMB IT WAS OBSERVED THAT THE NR 1 ENGINE STRUT OVERHEAT LIGHT CAME ON. IAW OPS CHECKLIST, SYSTEM CHECK CARRIED OUT AND FLIGHT CONTINUED WITHOUT INCIDENT. AFTER LANDING, INSPECTION WAS CARRIED OUT AND THE HIGH PRESSURE MODULATING AND SHUTOFF VAL
- [SDR CA040402006](https://openairdocs.org/sdr/CA040402006.md): Wire Harness · inoperative · Apr 1, 2004 · Boeing 727260 · Miscellaneous Wiring
  > (CAN) DURING START UP, IT WAS OBSERVED THAT AC PACK WATER SEPARATOR CB POPPED FOLLOWED BY A PACK TRIP. A BURNING ODRO WAS SENSED. ENGINES WERE SHUTDOWN. MAINTENANCE BEGAN INSPECTION AND COCKPIT LIGHTING BEGAN TO FLICKER. COCKPIT WAS FILLING WITH SMOKE. NR
- [SDR CA040209002](https://openairdocs.org/sdr/CA040209002.md): Window · cracked · Feb 5, 2004 · Boeing 727260 · Flight Compartment Windows
  > (CAN) DURING CLIMB, THE F/O OBSERVED THE R2 SLIDING WINDOW WAS CRACKED. THE DECISION WAS MADE TO RETURN TO BASE. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE R2 WINDOW ASSY WAS REPLACED IAW MM 56-12-11 AND CHECKED SERVICEABLE. THE R2 WINDOW HEAT CONTROLLER AND T
- [SDR CA040112003](https://openairdocs.org/sdr/CA040112003.md): Brake Pads · damaged · Jan 9, 2004 · Boeing 727260 · Brake
  > (CAN) DURING TAXI, CREW REPORTED THAT THERE WAS SOME DRAGGING FELT WHEN THE BRAKES WERE APPLIED. THE AIRCRAFT RETURNED TO THE BLOCKS. A DETAILED INSPECTION WAS CARRIED OUT AND NR 4 BRAKE WAS FOUND UNSERVICEABLE. THE BRAKE PADS WERE DAMAGED AND BROKEN. A SERVI
- [SDR CA031202003](https://openairdocs.org/sdr/CA031202003.md): Transponder · faulty · Nov 29, 2003 · Boeing 727260 · Emergency Locator Beacon
  > (CA) WAS NOTIFIED THAT SEARCH AND RESCUE WAS RECEIVING AN ELT RESPONSE FROM A COMPANY AIRCRAFT. INSPECTED AND IT WAS DETERMINED THIS AIRCRAFT WAS AT FAULT. THE UNIT WAS DISCONNECTED AND A FURTHER INSPECTION FOUND WATER LOCATED AROUND THE RECEPTACLE AND CONN
- [SDR CA031103002](https://openairdocs.org/sdr/CA031103002.md): Isolation Valve · failed · Oct 30, 2003 · Boeing 727260 · Air Distribution System
  > (CAN) DURING CLIMB, IT WAS OBSERVED THAT CABIN PRESSURE WAS NOT CONSISTENT WITH FLIGHT LEVEL. AIRCRAFT RETURNED TO BASE WITHOUT INCIDENT. AIRCRAFT WAS DISPATCHED UND ER MEL 21-01-01 WITH RT PACK INOP FLYING AT AN ALTITUDE OF FL 25,000 FT. THE ISOLATION VALVE W
- [SDR CA021114006](https://openairdocs.org/sdr/CA021114006.md): Bolt · cracked · Nov 12, 2002 · Boeing 727260 · Nose/Tail Landing Gear Attach Section
  > (CAN) AT C-CHECK. WHILE PERFORMING FWD MLG TRUNION FITTING REPLACEMENT ON THE RT MLG. TECH NOTICED NO SHIMS WERE INSTALLED BETWEEN FWD TRUNNION BEARING AND TRUNNION LINK TO OBTAIN REQUIRED 0.00 TO 0.003 INCH CLEARANCE. NO MEARSURMENT WAS TAKEN DUE TO FWD TRU
- [SDR CA020429002](https://openairdocs.org/sdr/CA020429002.md): Tie Bolt · sheared · Apr 26, 2002 · Boeing 727260 · Wheel/Ski/Float
  > (CAN) DURING AIRCRAFT SERVICE CHECK FOUND NR 3 MAIN WHEEL ASSEMBLY WITH ONE SHEARED TIE BOLT NR 3 MAIN WHEEL ASSEMBLY. REPLACED IAW MM 32-45-1. MAIN WHEEL ASSEMBLY TO BE SENT TO OVERHAUL FACILITY FOR INVESTIGATION AND TEAR DOWN REPORT. FURTHER REPORT(S) TO F
- [SDR CA020422005](https://openairdocs.org/sdr/CA020422005.md): Bolt · broken · Apr 18, 2002 · Boeing 727260 · Wheel/Ski/Float
  > (CAN) DURING SERVICE CHECK, NR 2 MAIN WHEEL TIRE FOUND DEEPLY CUT AND ONE TIE BOLT BROKEN ON MAIN WHEEL HUB ASSY. NR 2 MAIN WHEEL ASSY REPLACED PER MM. MAIN WHEEL ASSY TSO: 472.9 HRS. CSO: 354 CYCLES MAIN WHEEL ASSY TO BE SENT TO OVERHAUL FACILITY FOR TEAR D
- [SDR CA020412013](https://openairdocs.org/sdr/CA020412013.md): Hinge Pin · loose · Apr 8, 2002 · Boeing 727260 · Cargo/Baggage Doors
  > (CAN) DURING B CHECK INSPECTION, MAIN CARGO DOOR HINGE PIN WAS FOUND MIGRATING AFT APROX. 6 INCHES. HINGE PIN REPOSITIONED AND SAFETIED.
- [SDR CA020205007](https://openairdocs.org/sdr/CA020205007.md): Hinge Pin · corroded · Feb 4, 2002 · Boeing 727260 · Horizontal Stabilizer, Tab Structure
  > (CAN) DURING INSPECTION OF HORIZONTAL STABILIZER HINGE PINS, FOUND THE RT SIDE OUTER PIN THREADS AND THREAD RELIEF AREA CORRODED. THE OUTER AND INNER PINS WILL BE REPLACED PRIOR TO NEXT FLIGHT.
- [SDR CA020103007](https://openairdocs.org/sdr/CA020103007.md): Engine · failed · Dec 28, 2001 · Boeing 727260 · Turbine Engine Compressor Section
  > (CAN) NR 3 ENGINE SHUT DOWN IN FLIGHT DUE VIBRATION. REPAIR FACILITY EVALUATION: EXTENSIVE IMPACT DAMAGE WAS NOTED ON THE 7-12 STAGE STATOR VANES AND THE 7-13 STAGE BLADES. THIS DAMAGE APPEARS TO HAVE ORIGINATED FROM A FRACTURED 7 STAGE COMPRESSOR BLADE. TH
- [SDR CA011119003](https://openairdocs.org/sdr/CA011119003.md): Engine · failed · Nov 7, 2001 · Boeing 727260 · Engine (Turbine/Turboprop)
  > (CAN) ON DESCENT, THRUST AT IDLE, NR 3 START LEVER VIBRATED IN DETENT. NR 3 EGT 100 DEGREES HIGHER THAN ENGINES NR 1 AND 2. "WHINING NOISE" AND VIBRATION FELT IN FLOOR WHEN THRUST LEVER ADVANCED. ENGINE SHUT DOWN IN FLIGHT. BORESCOPE INSPECTION CARRIED OUT O
- [SDR CA010724026](https://openairdocs.org/sdr/CA010724026.md): Wheel · cracked · Jul 14, 2001 · Boeing 727260 · Wheel/Ski/Float
  > (CAN) DURING SERVICE CHECK, NR 1 MAIN WHEEL TIRE PRESSURE FOUND TO BE 40 PSI PRESSURE DETECTED TO BE LEAKING AT WHEEL HUB. NR 1 AND 2 MAIN WHEEL ASSEMBLIES REPLACED, NO FURTHER FAULTS AFTER 8 FLIGHT SEGMENTS.
- [SDR CA010628001](https://openairdocs.org/sdr/CA010628001.md): Wire · broken · Jun 19, 2001 · Boeing 727260 · Landing Gear System Wiring
  > (CAN) WHEN LANDING GEAR EXTENDED, R/H MAIN GEAR DOOR LIGHTS DO NO ILLUMINATE. INSPECTED RT MAIN GEAR DOOR CANNON PLUG, WIRE PIN 6 BROKEN, REPAIRED WIRE TO PIN 6. IAW WDM 32-60-04, CANNON PLUG RESECURED FUNCTION CHECKED SERVICABLE.
- [SDR CA000907027](https://openairdocs.org/sdr/CA000907027.md): Engine · failed · Aug 22, 2000 · Boeing 727260 · Engine/Transmission Coupling
  > (CAN) PRIOR TO DESCENT INTO YYC LOW OIL PRESSURE LIGHT ON FOR NR 2 ENGINE OIL PRESSURE DECREASING AND OIL QUANTITY DECREASING.ENGINE FAILURE AND SHUTDOWN FOLLOWED BY ONE ENGINE INOPERATIVE CHECKLIST CARRIED OUT. DECLARED EMERGENCY LANDING. TROUBLESHOOTING CAR
- [SDR CA000215019](https://openairdocs.org/sdr/CA000215019.md): Actuator · failed · Feb 4, 2000 · Boeing 727260 · Leading Edge Slat Actuator
  > (CAN) A/C TURNBACK DUE TO LE FLAP ACTUATOR WOULD NOT RETRACT. NR 2 LE FLAP INDICATES DOWN WHEN FLAP IN RETRACT POSITION. REPLACED.
- [SDR S84A008](https://openairdocs.org/sdr/S84A008.md): Transmitter · failed · Feb 3, 2000 · N901PG · Boeing 727260 · Trailing Flap Position Indicating System
  > ON TAXI OUT, SPLIT FLAP BETWEEN INBOARD AND OUTBOARD 0 DEGREES THROUGH 15 DEGREES. ADJUSTED LEFT OUTBOARD FLAP POSITION TRANSMITTER. OPS CHECK GOOD IAW MM 27-52-13. (M)
- [SDR S84A007](https://openairdocs.org/sdr/S84A007.md): Switch · leaking · Jan 28, 2000 · N901PG · Boeing 727260 · Engine Oil Quantity
  > NR 2 ENGINE QTY DECREASED TO ZERO. OIL PRESSURE DOWN TO 38 PSI OIL TEMP 80 DEGREES CELSIUS. ENGINE WAS SHUTDOWN AT 0158Z. ENGINE WINDMILLED AT 17 PSI 80 DEGREES CELSIUS FOR 15 MINUTES. SERVICED ENGINE OIL, MOTOR ENGINE AND FOUND OIL LEAKING FROM LOW OIL PR
- [SDR S84A006](https://openairdocs.org/sdr/S84A006.md): Warning Light · illuminated · Jan 22, 2000 · N901PG · Boeing 727260 · Engine Oil Indicating System
  > NR 2 ENGINE OIL BYPASS LIGHT ILLUMINATED, SHUTDOWN ENGINE PER AFM. DEFERRED AS PER MEL 79-2 ACCOMPLISHED DPPG 79-2. NO CONTAMINANTS FOUND ON INSPECTION OF OIL FILTER FILTER NEED TO BE INSPECTED EVERY 12 FLIGHT HOURS. (M)
- [SDR CA991209038](https://openairdocs.org/sdr/CA991209038.md): Line · misinstalled · Nov 6, 1999 · Boeing 727260 · Brake Anti-Skid Section
  > (CAN) ON ONE OCCASION BRAKE CHATTER APPEARS ON RT SIDE. FOUND TWO HYDRAULIC LINES CROSSED, REPAIRED.
- [SDR CA991209037](https://openairdocs.org/sdr/CA991209037.md): Fitting · cracked · Nov 1, 1999 · Boeing 727260 · Engine Mount Section
  > (CAN) NR 3 FORWARD ENGINE SUPPORT FITTING CRACKED, REPLACED. REF 97-05-08.
- [SDR CA991209036](https://openairdocs.org/sdr/CA991209036.md): Indicator · failed · Oct 27, 1999 · Boeing 727260 · Trailing Flap Position Indicating System
  > (CAN) COULD NOT RETRACT INBOARD FLAPS PAST 2, USED ALTERNATE FLAPS TO RETRACT, CONTINUED FLIGHT AND AT LANDING USED NORMAL SYSTEM WITHOUT INCIDENT, ON GROUND CYCLED TWICE NORMALLY. REPLACED FLAP POSITION INDICATOR PER MM.
- [SDR CA991007087](https://openairdocs.org/sdr/CA991007087.md): Bracket · cracked · Sep 25, 1999 · Boeing 727260 · Nose/Tail Landing Gear Attach Section
  > (CAN) NLG ACTUATOR UPPER SUPPORT BRACKET CRACKED AT TRUNNION SUPPORT LT AND RT LOWER ATTACH HOLES CRACKED. REPLACED.
- [SDR 2000ZZZX24](https://openairdocs.org/sdr/2000ZZZX24.md): Spar · corroded · Sep 7, 1999 · N901PG · Boeing 727260 · Wing Spar
  > SJO - REPAIRED LEFT WING FRONT SPAR LOWER CHORD PLATE LEADING EDGE BETWEEN FSS 124 AND FSS 152 DUE TO WEAR AND CORROSION IAW COOPESA EO COO-2-57-549-99 DATED 9-22-99, AND, BOEING FAX NR COO-5J0-99-00306 H, DATED 9-22-99, AND BOEING FAX NR M-7200-99-08778 DATED
- [SDR 99ZZZX3641](https://openairdocs.org/sdr/99ZZZX3641.md): Light · inoperable · Aug 16, 1999 · N901PG · Boeing 727260 · Emergency Lighting
  > VARIOUS FLOOR 'E' PATH LIGHTS INOPERABLE. RELAMPED 3 PATHWAY LIGHTS. OPS CHECKED GOOD.
- [SDR 99ZZZX3640](https://openairdocs.org/sdr/99ZZZX3640.md): Light · inoperable · Aug 16, 1999 · N901PG · Boeing 727260 · Emergency Lighting
  > EMERGENCY LIGHT (INTERIOR) OVER R2 GALLEY DOOR INOPERABLE. REMOVED AND REPLACED BATTERY PACK PN 9505-42, SN OFF 25262; S/N ON 7071.
- [SDR 99ZZZX3639](https://openairdocs.org/sdr/99ZZZX3639.md): Bulb · failed · Aug 16, 1999 · N901PG · Boeing 727260 · Emergency Lighting
  > ONE BULB INOPERABLE ON EMERGENCY LIGHT ON AFT CARGO DOOR. RELAMPED. OPS CHECKED GOOD.
- [SDR 99ZZZX3638](https://openairdocs.org/sdr/99ZZZX3638.md): Bulb · failed · Aug 16, 1999 · N901PG · Boeing 727260 · Emergency Lighting
  > ONE BULB INOPERABLE ON RIGHT OVERWING FORWARD EMERGENCY LIGHT. RELAMPED. OPS CHECK GOOD.
- [SDR CA990715029](https://openairdocs.org/sdr/CA990715029.md): Altimeter · failed · Jul 15, 1999 · Boeing 727260 · Altimeter, Barometric/Encoder
  > (CAN) FIRST OFFICER'S ALTIMETER READS 100 FEET HIGHER THAN CAPTAIN'S ALT AT DECISION HEIGHT. FO'S ALTIMETER REPLACED AND SERVICEABLE.
- [SDR CA990707059](https://openairdocs.org/sdr/CA990707059.md): Drive Unit · inoperative · Jun 29, 1999 · Boeing 727260 · Trailing Edge Flap Control System
  > (CAN) OUTBOARD FLAP ALTERNATE SYSYEM INOPERABLE. OUTBOARD FLAPS ALT DRIVE UNIT REPLACED.

Next page: https://openairdocs.org/model/boeing-727-260/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 aircraft_model_key = '727260'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-260/reports

---
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