# Service difficulty reports: N284KH, cancelled May 14, 2007

A list on [N284KH, cancelled May 14, 2007](https://openairdocs.org/deregistered/N284KH-2007-05-14.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 · 57 reports

- [SDR GAIA06027OP](https://openairdocs.org/sdr/GAIA06027OP.md): Shutoff Valve · closed · Aug 25, 2006 · N284KH · Boeing 7272J0 · Fuel Selector/Shut-Off Valve
  > DURING CLIMB THE NR 2 ENGINE OIL FILTER BYPASS/LOW PRESSURE LIGHT ILLUMINATED. THE OIL PRESSURE TEMPERATURE AND QUANTITY WERE NORMAL. THE NR 2 ENGINE FLAMED OUT SHORTLY AFTERWARD. THE FLIGHT CREW PERFORMED THE ENGINE FAILURE CHECKLIST AND RETURNED. THE AIR
- [SDR GAIA05019OP](https://openairdocs.org/sdr/GAIA05019OP.md): Light · illuminated · Apr 4, 2005 · N284KH · Boeing 7272J0 · Emergency Lighting
  > EMERGENCY EXIT DOOR LIGHT ON ALL THE TIME. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY. AIRCRAFT RETURNED TO SERVICE. (K)
- [SDR GAIA05016OP](https://openairdocs.org/sdr/GAIA05016OP.md): Battery Pack · discharged · Mar 25, 2005 · N284KH · Boeing 7272J0 · Emergency Lighting
  > DURING PREFLIGHT, FOUND L1 DOOR AND COCKPIT ENTRY DOOR EMERGENCY BATTERY PACKS DRAINED TO DIM ILLUMINATION. REPLACED BATTERY PACKS (2 EA). OPERATED EMERGENCY LIGHTS SYSTEM AND FOUND OPERATING NORMALLY. OK FOR SUBSEQUENT FLIGHT. AC WAS RETURNED TO SERVICE.
- [SDR GAIA05002OP](https://openairdocs.org/sdr/GAIA05002OP.md): O-Ring · damaged · Jan 18, 2005 · N284KH · Boeing 7272J0 · Turbine Engine Oil System
  > DURING CRUISE THE FLIGHT CREW SHUT DOWN THE NR 2 ENGINE DUE TO LOSS OF OIL QUANTITY AND PRESSURE. THE AIRCRAFT DIVERTED, AND MADE AN UNEVENTFUL LANDING. REMOVED AND REINSTALLED NR 2 ENGINE FUEL PUMP, REPLACED FUEL PUMP GARLOC SEAL AND SHAFT O-RING PACKING.
- [SDR GAIA04171OP](https://openairdocs.org/sdr/GAIA04171OP.md): Gasket · blown · Oct 19, 2004 · N284KH · Boeing 7272J0 · Engine Bleed Air System
  > DURING CLIMB, THE NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED, WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND BLOWN GASKET AND LOOSE CLAMPS AND DUCT LEAKS. REMOVED AND REPLACED GASKET AND TIGHTENED CLA
- [SDR GAIA04168OP](https://openairdocs.org/sdr/GAIA04168OP.md): Sequence Valve · cracked · Sep 30, 2004 · N284KH · Boeing 7272J0 · Landing Gear Retraction/Extension System
  > FLT 715 - ELP-FWA - ON TAKEOFF DURING GEAR RETRACTION THE FLIGHT CREW NOTICED THE A-SYSTEM HYDRAULIC QUANTITY WENT TO ZERO. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ELP WHERE A LANDING WAS MADE WITHOUT INCIDENT. FOUND LEFT MLG SEQUENCE VALVE LE
- [SDR GAIA02051ST](https://openairdocs.org/sdr/GAIA02051ST.md): Stringer · cracked · May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Main, Longeron/Stringer
  > DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STRINGER 15 LEFT IS CRACKED AT BS 720B PLUS 5. ACCOMPLISHED STRINGER REPAIR AT BS 720B PLUS 5 STRINGER 15 LEFT IAW B727 SRM 53-10-3 FIG 5. (M)
- [SDR GAIA02052ST](https://openairdocs.org/sdr/GAIA02052ST.md): Stringer · cracked · May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Main, Longeron/Stringer
  > DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STRINGER 15 LEFT IS CRACKED AT BS 720B PLUS 15. ACCOMPLISHED STRINGER REPAIR AT BS 720B PLUS 15 STRINGER 15 LEFT IAW B727 SRM 53-10-3 FIG 5. (M)
- [SDR GAIA02053ST](https://openairdocs.org/sdr/GAIA02053ST.md): Seat Track · damaged · May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach Fittings
  > DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE MAIN CABIN SEAT TRACK RBL 24.75 IS DAMAGED SEVERAL DIFFERENT PLACES FROM BS 480-530. ACCOMPLISHED SEAT TRACK REPAIR AT BS 480-530 RBL 24.75 IAW B727 SRM 53-10-5 FIG 1. (M)
- [SDR GAIA02054ST](https://openairdocs.org/sdr/GAIA02054ST.md): Stiffener · cracked · May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE PRESSURE BULKHEAD BS 1183 VERTICAL BEAM LBL 36.9 CRACKED AT WL 245. ACCOMPLISHED BS 1183 VERTICAL BEAM REPAIR AT LBL 36.9 IAW S/B 727-53-0192. (M)
- [SDR GAIA02055ST](https://openairdocs.org/sdr/GAIA02055ST.md): Skin · cracked · May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Main, Plate/Skin
  > DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE FUSELAGE SKIN IS CRACKED AT THE FORWARD ENTRY DOOR LOWER HINGE CUT OUT. ACCOMPLISHED FUSELAGE SKIN REPAIR AT THE FORWARD ENTRY DOOR LOWER HINGE CUT OUT IAW S/B 727-53-0198. (M)
- [SDR GAIA02056ST](https://openairdocs.org/sdr/GAIA02056ST.md): Web · corroded · May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT STATION 1230 AFT FACE OF THE TAIL SKIN CAVITY BULKHEAD, CORROSION ON SUPPORT ANGLE AND WEB VISIBLE THROUGH AIRSTAIR CUT-OUT, AFT OF THE TAIL SKID. ACCOMPLISHED BS 1230 WEB AND T-ANGLE REPAIR IAW B727 SRM 51-
- [SDR GAIA02057ST](https://openairdocs.org/sdr/GAIA02057ST.md): Web · cracked · May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous Structure
  > DURING A CHECK INSPECTION, IT WAS DISCOVERED THAT VENTRAL STAIR AREA STATION 1225 LBL 12, VERTICAL WEB HAS A CRACK AT THE LIGHTENING HOLE. ACCOMPLISHED BS 1225, LBL 12 WEB REPAIR IAW B727 SRM 51-40-2 FIG 1. (M)
- [SDR GAIA02058ST](https://openairdocs.org/sdr/GAIA02058ST.md): Web · cracked · May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT VENTRAL STAIR AREA STATION 1232 LBL 14, VERTICAL WEB IS BUCKLED WITH A 3 INCH CRACK OUTBOARD OF 5TH STEP FROM TOP. ACCOMPLISHED BS 1232, LBL 14 CRACKED WEB ANGLE REPLACEMENT IAW B727 SRM 53-10-2 FIG 6. (M)
- [SDR GAIA02059ST](https://openairdocs.org/sdr/GAIA02059ST.md): Web · cracked · May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THAT THE VENTRAL STAIR AREA STATION 1244 RBL 12 VERTICAL WEB HAS 1 CRACK AT THE LIGHTENING HOLE. ACCOMPLISHED TORQUE BOX WEB REPAIR IAW B727 SRM 51-40-2 FIG 1. (M)
- [SDR GAIA02060ST](https://openairdocs.org/sdr/GAIA02060ST.md): Spar · corroded · May 17, 2002 · N284KH · Boeing 7272J0 · Wing Spar
  > DURING A C-CHECK INSPECTION AT FLIGHTSTAR, IT WAS DISCOVERED LEFT WING FRONT SPAR LOWER CHORD IS CORRODED UNDER AND INBOARD OF EXISTING REPAIR INSIDE L/E COVE AREA AT LES 200-240. ACCOMPLISHED LEFT WING LEADING EDGE LOWER SKIN AND SPAR CHORD REPAIR IAW AVITAS
- [SDR GAIA02061ST](https://openairdocs.org/sdr/GAIA02061ST.md): Spar · corroded · May 17, 2002 · N284KH · Boeing 7272J0 · Wing Spar
  > DURING A C-CHECK INSPECTION AT FLIGHT STAR, IT WAS DISCOVERED LEFT WING FRONT SPAR UPPER SURFACE AT WS 410 IS CORRODED. ACCOMPLISHED LEFT WING FRONT SPAR LOWER CHORD UPPER SURFACE REPAIR IAW B727 SRM 57-30-4 FIG 6. (M)
- [SDR GAIA02062ST](https://openairdocs.org/sdr/GAIA02062ST.md): Hinge · cracked · May 17, 2002 · N284KH · Boeing 7272J0 · Cargo/Baggage Doors
  > DURING A C-CHECK INSPECTION, IT WAS DISCOVERED THE MAIN CARGO DOOR HINGE AFT UPPER SECTION IS CRACKED. ACCOMPLISHED MAIN CARGO DOOR HINGE UPPER AFT SECTION REPLACEMENT IAW B727-200 MM AEI STC SA179SO. (M)
- [SDR GAIA02063ST](https://openairdocs.org/sdr/GAIA02063ST.md): Intercostal · cracked · May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, IT WAS DISCOVERED IN THE AFT CARGO COMPARTMENT BETWEEN BS 1030 AND 1050 AT STRINGER 25L, INTERCOSTAL IS CRACKED. ACCOMPLISHED INTERCOSTAL REPLACEMENT IAW B727 SRM 53-10-2 FIG 5. (M)
- [SDR GAIA02064ST](https://openairdocs.org/sdr/GAIA02064ST.md): Intercostal · cracked · May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous Structure
  > DURING A C-CHECK INSPECTION, IT WAS DISCOVERED IN THE FORWARD CARGO COMPARTMENT, INTERCOSTAL IS CRACKED BETWEEN BS 950A-950B AT STRINGER 25L. ACCOMPLISHED INTERCOSTAL REPAIR IAW B727 SRM 51-40-3 FIG 1. (M)
- [SDR GAIA02065ST](https://openairdocs.org/sdr/GAIA02065ST.md): Stringer · cracked · May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Main, Longeron/Stringer
  > DURING A C-CHECK INSPECTION, IT WAS DISCOVERED STRINGER 18A RIGHT IS CRACKED AT BS 940 RUNNING AFT FROM RADIUS BLOCKS AT THE BASE OF THE HORIZONTAL LEG. ACCOMPLISHED STRINGER 18A REPAIR IAW BOEING DRAWING 65C27166. (M)
- [SDR GAIA02066ST](https://openairdocs.org/sdr/GAIA02066ST.md): Skin · corroded · May 17, 2002 · N284KH · Boeing 7272J0 · Fuselage Main, Plate/Skin
  > DURING A C-CHECK INSPECTION, IT WAS DISCOVERED DISHED FASTENERS ON FUSELAGE SKIN AT BS 351, BELOW STRINGER 26R. ACCOMPLISHED SKIN PANEL AND T-CHORD REPLACEMENT IAW B727 SRM 53-30-2, FIG 2 AND SRM 51-30-2. (M)
- [SDR GAIA01126ST](https://openairdocs.org/sdr/GAIA01126ST.md): Doubler · leaking · Apr 13, 2001 · N284KH · Boeing 7272J0 · Wing, Plate/Skin
  > DURING A ROUTINE INSPECTION, IT WAS DISCOVERED THAT THE LEFT WING AT STATION 224.5 HAD A PREVIOUS DOUBLER REPAIR THAT WAS LEAKING FUEL FROM SEVERAL HI-LOCKS FASTENERS. REMOVED AND REPLACED DOUBLER IAW KHA EA B7-57-025. FLIGHT VEHICLES CONSULTING DRAWING 57-0
- [SDR GAIA00795](https://openairdocs.org/sdr/GAIA00795.md): Switch · out of adj · Dec 22, 2000 · N284KH · Boeing 7272J0 · Leading Edge Slat Position Indicating System
  > NR2 LEADING EDGE FLAP DEPLOYED IN FLIGHT. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT ANY FURTHER DIFFICULTIES.ADJUSTED NR2 LEADING EDGE FLAP SWITCH, ONE TURN AND RESAFETIED. OPS CHECKED GOOD ON GROUND. AIRCRAFT RETURNED TO SERVICE.
- [SDR GAIA00524](https://openairdocs.org/sdr/GAIA00524.md): Door · malfunctioned · Sep 20, 2000 · N284KH · Boeing 7272J0 · Landing Gear Door Retract Section
  > FLT 1729 - DEN-FWA - AFTER TAKEOFF, THE GEAR HANDLE WOULD NOT GO PAST OFF, GEAR AND DOORS LIGHTS WERE ALL ILLUMINATED. CYCLED THE GEAR THREE TIMES AND THERE WAS NO CHARGE. THE AIRCRAFT RETURNED TO DEN AND LANDED WITHOUT ANY FURTHER DIFFICULTIES. JACKED AIRC
- [SDR GAIA0088](https://openairdocs.org/sdr/GAIA0088.md): Battery · discharged · Feb 14, 2000 · N284KH · Boeing 7272J0 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE AT HNL, IT WAS DISCOVERED THAT THE EMERGENCY EXIT LIGHTS WOULD NOT RETAIN A CHARGE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERIES. OPERATIONAL CHECKS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)
- [SDR GAIA9974](https://openairdocs.org/sdr/GAIA9974.md): O-Ring · deteriorated · Jun 16, 1999 · N284KH · Boeing 7272J0 · Fuel Controlling System
  > DURING BOS-TOL - FLT 715 - DURING DESCENT AT FL280, THE FLIGHT CREW NOTICED THAT THE NR 1 ENGINE WOULD ONLY PRODUCE PARTIAL POWER. THE FLIGHT CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN ON THE NR 1 ENGINE AND DECLARED AN EMERGENCY. THE AIRCRAFT CONTINUED
- [SDR GAIA9973](https://openairdocs.org/sdr/GAIA9973.md): Connector · dirty · Jun 8, 1999 · N284KH · Boeing 7272J0 · Leading Edge Slat Position Indicating System
  > FLT 504 - DURING CLIMB-OUT FROM TOL, THE NR 5 SLAT INDICATE AS NOT RETRACED WHILE ALL OTHER TRAILING AND LEADING EDGE DEVICES WERE RETRACTED. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO TOL. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. CLEANED NR 5 S
- [SDR GAIA9997](https://openairdocs.org/sdr/GAIA9997.md): Pitot Tube · clogged · Jun 7, 1999 · N284KH · Boeing 7272J0 · Pitot/Static System
  > AFTER TAKEOFF FROM AUS TO STL, FLIGHT 721, HAD THE CO-PILOTS AIRSPEED INDICATOR DECREASE 40 TO 50 KNOTS FROM THE CAPTAINS AIRSPEED INDICATOR. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO AUS. THE AIRCRAFT LANDED WITHOUT FURTHER PROBLEMS. FOUND AN OBSTR
- [SDR GAIA9960A](https://openairdocs.org/sdr/GAIA9960A.md): Pin · missing · May 27, 1999 · N284KH · Boeing 7272J0 · Nose/Tail Landing Gear
  > MCO - FLT 1726 - AFTER TAKEOFF, RETRACTED GEAR AND GEAR DOOR LIGHT REMAINED ON. RECYCLED GEAR AND LIGHT REMAINED ON. PROCEEDED TO MEM AND LANDING WAS SMOOTH. BRAKING WAS STARTED AT 80 KIS, RUMBLE WAS NOTICED IN THE AIRCRAFT. UNABLE TO STEER AIRCRAFT. AIRC
- [SDR 98ZZZX2710](https://openairdocs.org/sdr/98ZZZX2710.md): B Nut · loose · Jul 2, 1998 · N284KH · Boeing 7272J0 · Hydraulic System, Main
  > AIRCRAFT DIVERTED INTO KFLL DUE LOSS OF A-SYSTEM HYDRAULIC FLUID: FOUND B-NUT NR 1 ENGINE MAIN HYD LINE LOOSE. TIGHTENED B-NUT. CHECKED CASE DRAIN FITTINGS. PRESSURE CHECKED SYSTEM. RELEASED AIRCRAFT.
- [SDR 98ZZZX2546](https://openairdocs.org/sdr/98ZZZX2546.md): B-Nut · loose · Jul 2, 1998 · N284KH · Boeing 7272J0 · Hydraulic System, Main
  > AIRCRAFT DIVERTED INTO KFLL. DUE LOSS OF A-SYSTEM HYDRAULIC FLUID, FOUND B-NUT NR 1 ENGINE MAIN HYDRAULIC LINE LOOSE. TIGHTENED B-NUT, CHECKED CASE DRAIN FITTINGS. PRESSURE CHECKED SYSTEM. RELEASE AIRCRAFT.
- [SDR B4MR97031](https://openairdocs.org/sdr/B4MR97031.md): Skin · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Wing, Plate/Skin
  > DURING ROUTINE C-CHECK INSPECTION, FOUND LFT WING, O/B MID FLAP, L/E LWR SURFACE, CORROSION ON TWO AREAS. (REFERENCE: O/B ATTACHED FAIRING FWD AREA). REPAIRED IAW ENGINEERING SKETCH NR AIA/E/2587, APPROVED BY FAA FORM 8110-3 DATED 7-21-97 PN=7075-T6 0.125IN.
- [SDR B4MR97030](https://openairdocs.org/sdr/B4MR97030.md): Angle · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Miscellaneous Structure
  > DURING ROUTINE C-CHECK INSPECTION, FOUND LEFT MLG WW, AFT BULKHEAD LWR CENTER AREA, CORROSION ON T-ANGLE. REMOVED CORROSION ON T-ANGLE, FOUND TO BE OUT OF LIMITS IAW B727 SRM 53-10-1. REMOVED DAMAGED AREA, REPAIRED T-ANGLE IAW B727 SRM 51-40-4, 51-30-2 AND M
- [SDR B4MR97029](https://openairdocs.org/sdr/B4MR97029.md): Structure · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Wing Main, Frame Structure
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND LT WING L/E AREA, NR 2 L/E FLAP STA 212 HAS SUPPORT ANGLE WEB CORRODED AND CORROSION AROUND ANCHOR NUTS. FOUND CORROSION TO BE OUT OF LIMITS IAW B727 SRM 57-20-1. REMOVED AND REPLACED ACCESS WEBBING PANEL, TOP COVE
- [SDR B4MR97028](https://openairdocs.org/sdr/B4MR97028.md): Floorbeam · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Main, Floor Beam
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND STA 328 FLOORBEAM AT LBL 3 HAS CORROSION. REPAIRED FLOORBEAM IAW B727 SRM 53-10-8 FIG 3. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 110399.
- [SDR B4MR97027](https://openairdocs.org/sdr/B4MR97027.md): Seat Track · worn · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND FE SEAT TRACK IS WORN. REPLACED FE SEAT TRACK IAW B727 BOEING MM CHAPTER 25-10-81. CORROSION TASK CARD NUMBER C53-221-01. NON-ROUTINE TASK CARD NUMBER 110442.
- [SDR B4MR97026](https://openairdocs.org/sdr/B4MR97026.md): Skin · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Main, Plate/Skin
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND TOP RT ELEVATOR ES92 AREA HAS SURFACE CORROSION OUT OF LIMITS. REPAIRED AND REPLACED A PIECE OF TOP SKIN IAW B727 SRM 55-20-3 FIG 2 PN=2024-T3.032. CORROSION TASK CARD NUMBER C55-300-10. NON-ROUTINE TASK CARD NUM
- [SDR B4MR97025](https://openairdocs.org/sdr/B4MR97025.md): Skin · corrosion · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Main, Plate/Skin
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND FORWARD PIT FS 686 S26R TO 25R HAS SURFACE CORROSION ON INTERNAL SKIN. CORROSION OUT OF LIMITS IAW B727 SRM 53-30-1. REPAIRED IAW SRM 53-30-3 FIG 5 PN=2024-T3. CORROSION TASK CARD NUMBER C53-113-01. NON-ROUTINE T
- [SDR B4MR97024](https://openairdocs.org/sdr/B4MR97024.md): Skin · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Main, Plate/Skin
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND RT MLG W/W OUTBD, ABOVE MLG BEAM, BETWEEN STA 930 AND 940 PRESSURE DECK SKIN AND FASTENERS HAVE CORROSION. REPAIRED AREA (CORROSION OUT OF LIMITS IAW B727 SRM 53-10-1) IAW SRM 53-10-9 FIG 4 PN=2024-T3. CORROSION TA
- [SDR B4MR97023](https://openairdocs.org/sdr/B4MR97023.md): Support · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Flight Compartment Equipment
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND COCKPIT AREA, CO-PILOT SEAT BASE SUPPORT NEEDING ANTI CORROSION TREATMENT ON BOTH AFT ATTACH POINTS. REMOVED AND REPLACED CO-PILOT SEAT BASE SUPPORT IAW BOEING B727 MM CHAPTER 25-10-42. NEW BASE SUPPORT REQUIRED DU
- [SDR B4MR97022](https://openairdocs.org/sdr/B4MR97022.md): Keel Beam · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Main, Keel
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND KEEL BEAM RT W/W UNDER APU ANGLE CORRODED TOP AND BOTTOM. OUT OF LIMITS PER SRM 53-10-1. REPAIRED PER SRM 51-40-4 PN=7075-T6 OR 2X2X.150. CORROSION TASK CARD NUMBER C53-132-01. NON-ROUTINE TASK CARD NUMBER 108224
- [SDR B4MR97021](https://openairdocs.org/sdr/B4MR97021.md): Seat Track · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND SEAT TRACK LBL 40 STA 1140 TO 1030 CORRODED. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C53-111-01. NON-ROUTINE TASK CARD NUMBER 108166.
- [SDR B4MR97020](https://openairdocs.org/sdr/B4MR97020.md): Seat Track · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND SEAT TRACK LBL 20 STA 1140 TO 1030 CORRODED. REPAIRED SEAT TRACK PER B727 SRM 53-10-5 CORROSION WAS FOUND TO BE OUT OF LIMITS PER SRM 51-10-2. CORROSION TASK CARD NUMBER C53-111-01. NON-ROUTINE TASK CARD NUMBER 108
- [SDR B4MR97019](https://openairdocs.org/sdr/B4MR97019.md): Seat Track · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND SEAT TRACK RBL 20 STA 1140 TO 1030 CORROSION. REPAIRED SEAT TRACK PER B727 SRM 53-10-5 CORROSION WAS FOUND TO BE OUT OF LIMITS PER SRM 51-10-2. CORROSION TASK CARD NUMBER C53-111-01. NON-ROUTINE TASK CARD NUMBER 1
- [SDR B4MR97018](https://openairdocs.org/sdr/B4MR97018.md): Seat Track · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND SEAT TRACK RBL 40 STA 1140 TO 1030 CORROSION. REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C53-111-01. NON-ROUTINE TASK CARD NUMBER 108163.
- [SDR B4MR97017](https://openairdocs.org/sdr/B4MR97017.md): Seat Track · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND STA 1050 TO 1070 LBL 40 SEAT TRACK CORRODED (OLD REPAIR). REMOVED AND REPLACED SEAT TRACK IAW B727 SRM 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK CARD NUMBER 107834.
- [SDR B4MR97016](https://openairdocs.org/sdr/B4MR97016.md): Seat Track · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage, Seat/Cargo Attach Fittings
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND STA 1070 TO 1090 RBL 46 SEAT TRACK CORRODED AROUND NUT PLATE AND BETWEEN TRACK AND FLOORBEAM. REMOVED AND REPLACED SEAT TRACK IAW B727 51-10-1 AND 51-30-2. CORROSION TASK CARD NUMBER C53-224-01. NON-ROUTINE TASK C
- [SDR B4MR97015](https://openairdocs.org/sdr/B4MR97015.md): Heat Plenem · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Heating System
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND HEAVY CORROSION LT HEAT EXCHANGER PLENEM TOP PLATE AFT END REPAIR PREVIOUSLY ACCOMPLISHED IS CORRODED. ALSO, REPAIRED DAMAGE AREA IAW BOEING REPORT KHC-ORD-97-0003RR DATED 9-JUL-97, APPROVED BY FAA FORM 8110-3 DATED
- [SDR B4MR97014](https://openairdocs.org/sdr/B4MR97014.md): Skin · corroded · Sep 26, 1997 · N284KH · Boeing 7272J0 · Fuselage Main, Plate/Skin
  > DURING ROUTINE CPCP CHECK INSPECTION, FOUND STA 1090R FWD EDGE OF NR 3 CARGO DOOR OPENING HAS CORROSION UNDER LOWER END OF SKIN DOUBLER APPROX STR 25R. REMOVED AND REPLACED RT SKIN FROM STA 1010 TO 1090, STR 20 TO 26 IAW B727 SRM 51-10-1 AND 51-30-2 AND INSTA

Next page: https://openairdocs.org/deregistered/N284KH-2007-05-14/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 = 'N284KH' AND deregistration_id = 'N284KH-2007-05-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N284KH-2007-05-14/reports

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