# Service difficulty reports: N702DH, cancelled Sep 20, 2013

A list on [N702DH, cancelled Sep 20, 2013](https://openairdocs.org/deregistered/N702DH-2013-09-20.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 4 · 162 reports

- [SDR DHL2001702014](https://openairdocs.org/sdr/DHL2001702014.md): Connector · contaminated · Jul 17, 2001 · N702DH · Boeing 72730C · Auto Flight System Wiring
  > AUTOPILOT IS INOPERATIVE IN ALL ROLL MODES AIRCRAFT ROLLED HARD TO LEFT IN MANUAL MODE AND WAS UNRESPONSIVE TO INPUTS. CLEANED OXIDATION FROM ROLL SERVO CANNON PLUG CONTACTS. OPS CHECK OF AUTOPILOT GOOD PER MM 22-00.
- [SDR DHL2001702013](https://openairdocs.org/sdr/DHL2001702013.md): Autopilot Sys · intermittent · Jul 17, 2001 · N702DH · Boeing 72730C · Autopilot System
  > AUTOPILOT ROLL CONTROL INTERMITTENT. WHEN MALFUNCTIONING AUTO PILOT ENGAGES AND ROLLS SHARPLY UNCOMMANDED. CANNOT DUPLICATE, NO HISTORY. FOUND OPS CHECK GOOD ON GROUND IAW 727 MM 22-11-01.
- [SDR DHL2001702012](https://openairdocs.org/sdr/DHL2001702012.md): Switch · dirty · May 18, 2001 · N702DH · Boeing 72730C · Trailing Flap Position Indicating System
  > UPON CLEARANCE FOR TAKEOFF, ADVANCED THRUST LEVER T/O CONFIG WARNING HORN SOUNDED (REF - SPEEDBRAKE WAS STOWED, TRIM SET FLAPS WERE 15 - 15 GREEN). CLEANED FLAP WARNING SWITCH CYCLED FLAPS TO 15 DEG. OPS CK GOOD. NO HORN AND RESET FLAPS TO 0 DEG.
- [SDR DHL2001702011](https://openairdocs.org/sdr/DHL2001702011.md): Warning System · malfunctioned · May 12, 2001 · N702DH · Boeing 72730C · Central Warning
  > REJECTED T/O IN ROC DUE TO T/O WARNING HORN. WE DEPART RUNWAY. RESET CONTROLS. ON NEXT ATTEMPT, NO FURTHER PROBLEMS. TESTED TAKEOFF WARNING SYSTEM PER MM 31-26-1. OPS CHECK GOOD.
- [SDR DHL2001702010](https://openairdocs.org/sdr/DHL2001702010.md): Switch · stuck · Apr 24, 2001 · N702DH · Boeing 72730C · Trailing Edge Flap Control System
  > TAKEOFF WARNING HORN SOUNDED WHEN TAKEOFF THRUST WAS APPLIED WITH FLAPS AT 15, SPEED BRAKE STOWED, AND STAB TRIM AT 5.5. TAKEOFF WAS DISCONTINUED. FOUND TAKEOFF WARNING SWITCH STUCK. REMOVED AND REPLACED SWITCH. TESTED SYSTEM IAW DHL MM 27-51-191.
- [SDR DHL2001702009](https://openairdocs.org/sdr/DHL2001702009.md): Switch · out of adj · Apr 11, 2001 · N702DH · Boeing 72730C · Drag Control System
  > TAKEOFF WARNING HORN SOUNDED DURING T/O ROLL 60 KTS. TAKEOFF REJECTED. VERIFIED T/O CONFIGURATION WAS CORRECTED. 2ND T/O NORMAL. FOUND SPEED BRAKE TAKEOFF WARNING SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH S194 AND TESTED IAW MM 31-26-25 P401-403. OPS CH
- [SDR DHL2001702007](https://openairdocs.org/sdr/DHL2001702007.md): Windshield · failed · Mar 30, 2001 · N702DH · Boeing 72730C · Passenger/Crew Doors
  > L-2 WINDSHIELD CRACKED DURING CRUISE FLIGHT. CORRECTIVE ACTION: REPLACED L-2 WINDOW IAW B727 MM 56-12-11. OPS CK SERVICABLE PRESSURIZED A/C ON GROUND. NO LEAKS NOTED. STATUS CLOSED.
- [SDR DHL2001702008](https://openairdocs.org/sdr/DHL2001702008.md): Gearbox · leaking · Mar 29, 2001 · N702DH · Boeing 72730C · Accessory Gearboxes
  > IN CRUISE FLIGHT LOW OIL PRESS LIGHT ILLUMINATED. OIL PRESSURE FLUCTUATING BETWEEN 20-40 PSI. PERFORMED OIL PRESS BELOW 40 PSI ABNORMAL CHECKLIST AND DISCOVERED ZERO OIL QUANTITY. PERFORMED IN FLIGHT ENG SHUTDOWN ABNORMAL PROCEDURE. OIL PRESS INDICATION ZE
- [SDR DHL2001702006](https://openairdocs.org/sdr/DHL2001702006.md): Bolt · sheared · Mar 23, 2001 · N702DH · Boeing 72730C · Cargo/Baggage Doors
  > MAIN CARGO DOOR WILL NOT CLOSE.CORRECTIVE ACTION: REPLACED SHEARED BOLTS AT FWD CAM LATCH PER MM 52-34-21. OPS CHECK GOOD. STATUS CLOSED.
- [SDR DHL2001702003](https://openairdocs.org/sdr/DHL2001702003.md): Pump · failed · Mar 2, 2001 · N702DH · Boeing 72730C · Engine Fuel Pump
  > NR 2 ENGINE FAILURE ON TAKEOFF ROLL AT 90 KTS. REMOVED AND REPLACED FUEL PUMP. FUEL CONTROL UNIT CHECKS GOOD PER M/M 73-11-1 & 72-00.
- [SDR DHL2001702004](https://openairdocs.org/sdr/DHL2001702004.md): Floorbeam · corroded · Feb 17, 2001 · N702DH · Boeing 72730C · Fuselage Main, Floor Beam
  > AT FS 1050 LBL 3 ON BOTTOM OF FLOORBEAM WL 200 CORROSION ON FLOORBEAM AND GILLINER ATTACH ANGLE. REMOVED AND REPLACED LOWER SUPPORT TEE.
- [SDR DHL2001702005](https://openairdocs.org/sdr/DHL2001702005.md): Seat Track · damaged · Feb 17, 2001 · N702DH · Boeing 72730C · Fuselage, Seat/Cargo Attach Fittings
  > SIDE BASH BAR NR 3 AND 4 MUSHROOM OUT OF FLOOR TRACK. REMOVED AND REPLACED FLOOR TRACK FROM STA 480 TO 560 PER SRM 53-10-2 AND 53-10-5.
- [SDR DHL2001702002](https://openairdocs.org/sdr/DHL2001702002.md): Warning System · false activation · Jan 30, 2001 · N702DH · Boeing 72730C · Central Warning
  > DISCONTINUED TAKEOFF DUE TO TAKEOFF WARNING HORN. FLAPS, SPEEDBRAKE AND TRIM ALL PROPERLY SET. PERFORMED T/O WARN TEST PER MM 31-26-0 PARA 6, TEST OK.
- [SDR DHL2001702001](https://openairdocs.org/sdr/DHL2001702001.md): Warning System · activated · Jan 6, 2001 · N702DH · Boeing 72730C · Central Warning
  > RTO BECAUSE OF FALSE T/O WARNING HORN-RECYCLED FLAPS, WARNING DID NOT SOUND WHEN T/L ADVANCED. PREFORMED T/O WARNING TEST,FOUND NORMAL OPS PER M/M 34-00 AND 31-00
- [SDR DHL2000702003](https://openairdocs.org/sdr/DHL2000702003.md): Transmitter · stuck · Oct 19, 2000 · N702DH · Boeing 72730C · Engine Oil Indicating System
  > NR 3 ENGINE OIL PRESSURE INDICATION STUCK AT 10 PSI. REMOVED AND REPLACED NR 3 ENGINE OIL PRESSURE TRANSMITTER IAW M/M 79-32-1.
- [SDR DHL2000702002](https://openairdocs.org/sdr/DHL2000702002.md): Cam · cracked · Feb 18, 2000 · N702DH · Boeing 72730C · Cargo/Baggage Doors
  > MAIN CARGO DOOR SUPPORT CENTERING CAM CRACKED. INSTALLED CAM PER 53-30-0.
- [SDR DHL2000701001](https://openairdocs.org/sdr/DHL2000701001.md): Cam · cracked · Feb 18, 2000 · N702DH · Boeing 72730C · Cargo/Baggage Doors
  > MAIN CARGO DOOR SUPPORT CENTERING CAM CRACKED. INSTALLED CAM PER 53-30-0.
- [SDR DHL20007020](https://openairdocs.org/sdr/DHL20007020.md): Pin · installed · Feb 4, 2000 · N702DH · Boeing 72730C · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, GEAR WOULD NOT RETRACT. RETURNED FOR LANDING AND FOUND GEAR PINS INSTALLED
- [SDR DHL2000702001](https://openairdocs.org/sdr/DHL2000702001.md): Pin · installed · Feb 4, 2000 · N702DH · Boeing 72730C · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, GEAR WOULD NOT RETRACT. RETURNED FOR LANDING AND FOUND GEAR PINS INSTALLED.
- [SDR DHL99702001](https://openairdocs.org/sdr/DHL99702001.md): Bolt · loose · Aug 31, 1999 · N702DH · Boeing 72730C · Leading Edge Slat Control System
  > WHEN SELECTING FLAP 2 DEGREE UPON FLAP RETRACTION, AMBER L/E LIGHT FAILED TO EXTINGUSH. NO AMBER L/E LIGHTS ON S/O AUX PANEL WERE ILLUMINATED. FOUND AND SECURED 1 THROUGH BOLT ON FLAP DETENT SWITCH. CHECKED ADJUSTMENT AND OPS CHECK GOOD.
- [SDR DHL9970203C](https://openairdocs.org/sdr/DHL9970203C.md): Frame · cracked · Jun 30, 1999 · N702DH · Boeing 72730C · Engine Cowling System
  > C CHECK, NR 1 ENGINE UPPER COWLING NR 14 FRAME HS EVIDENCE OF HEAVY CHAFING UNDER IMPROPER STRAP REPAIR AT 1/B FLANGE, AT O/B AFT CORNER OF COWL. REMOVED REPAIR, INSTALLED REPAIR PER SRM 54-10-3, 6 BY 3 N/R 6095.
- [SDR DHL9970244C](https://openairdocs.org/sdr/DHL9970244C.md): Seat Track · cracked · Jun 26, 1999 · N702DH · Boeing 72730C · Fuselage, Seat/Cargo Attach Fittings
  > C CHECK, LWR AFT CARGO COMPARTMENT RT SEAT TRACK CRACK AT BOTH FWD AFT ENDS. REPLACED DAMAGE SECTION OF SEAT TRACK FROM STA 950 TO STA 1030; INSTALLED REPAIR AT STA 1030 AS PER B7272 SRM 53-10-5 FIG 8 MAT USED BAC1520-843 80 LOT NR 148462-1 PO NR 8314055; REP
- [SDR DHL9970214C](https://openairdocs.org/sdr/DHL9970214C.md): Skin · cracked · Jun 25, 1999 · N702DH · Boeing 72730C · Fuselage Main, Plate/Skin
  > C-CHECK, CRACK INDICATION AT FASTENER ONE INCH RIGHT OF (BLO) STA 480. CUT-OUT DAMAGED AREA OF SKIN AT FWD SIDE STA 480 PRODUCTION BREAK BETWEEN BLO AND STR 28R 4.0 BY 2.0 IAW B727 S/B 727-53-0084 DRAWING NO69-62161 SHEET 2. ALODINED AND PRIMED AREA IAW B727
- [SDR DHL9970211C](https://openairdocs.org/sdr/DHL9970211C.md): Skin · corroded · Jun 25, 1999 · N702DH · Boeing 72730C · Fuselage Main, Plate/Skin
  > C CHECK, PLUS 10 PERCENT MATERIAL LOSS AT STA 259 CIRCUIT BUTT SEAM APPRX S-9L LOCTION. INSTALLED DOUBLER REPAIR AT BS 259 STR 9L PER B727 S/B 727-53-0084 ALODINED AND PRIMED ALL PARTS AND AREA PER B727 SRM 51-10-2 MAT USED. FILLER.050 2024T3 21 BY 4 APPROX
- [SDR DHL9970235C](https://openairdocs.org/sdr/DHL9970235C.md): Skin · cracked · Jun 24, 1999 · N702DH · Boeing 72730C · Aileron Tabs
  > C CHECK, RT WING O/B AILERON, I/B UPPER SKIN CRACKED AT I/B TAB BOND WIRE ATTACHMENT FASTENER. REMOVED AILERON TAB, CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR 5 BY 7 PER SRM 57-50-5. BALANCEED PER SRM 51-80-4. NO WEIGHT REQUIRED. N/R 2103.
- [SDR DHL9970221C](https://openairdocs.org/sdr/DHL9970221C.md): Fitting · cracked · Jun 24, 1999 · N702DH · Boeing 72730C · Drag Control Actuator
  > C CHECK NR 6 SPOILER ACTUATOR SUPPORT FITTING IS CRACKED AT TOP FLANGE. CUT OUT DAMAGED AREAS I/B AND O/B SIDE OF NR 6 SPOILER ACT FITTING IAW AVITAS ENG. REPAIR ORDER NR 99AVHM.045R0-1 REV 1R SIZE OF CUT OUT 1 BY 1.5. EDDY CURRENT PER B727 NDT MAN. PART 6
- [SDR DHL9970216C](https://openairdocs.org/sdr/DHL9970216C.md): Ange · cracked · Jun 24, 1999 · N702DH · Boeing 72730C · Nacelle/Pylon Structure
  > C CHECK, NR 2 ENG PYLON, ANGLE CRACKED AT AFT OF ENG-MOUNT. REMOVED ANGLE AT NR 2 ENG PYLON AT AFT OF ENG MOUNT IAW B727 SRM 51-30-2. REPLACED ANGLE AT NR 2 ENG PYLON AT AFT OF ENG MOUNT. MAT USES 7075-00. 050. PO NR 8315267 LO NR 219081 SIZED 8 BY 3 IAW B7
- [SDR DHL9970245C](https://openairdocs.org/sdr/DHL9970245C.md): Web · corroded · Jun 23, 1999 · N702DH · Boeing 72730C · Fuselage Miscellaneous Structure
  > C-CHECK, MAIN CABIN SHEAR WEB PLATE HAS CORROSION BELOW THE PLATE BS 1176 LBL 26. REMOVED FASTENERS ON HAT CHANNEL ANGLE AT BS 1176 LBL26 AS PER SRM 51-30-2. CUTOUT DAMAGE CORRODED AREA AS PER 727 SRM 51-40-2 SIZE CUT OUT 14 BY 15. INSTALLED A WEB REPAIR AS
- [SDR DHL9970242C](https://openairdocs.org/sdr/DHL9970242C.md): Bracket · cracked · Jun 23, 1999 · N702DH · Boeing 72730C · Wing Miscellaneous Structure
  > C-CHECK, RT WING T/E COVE PNL SUPPORT BRACKET CRACK AT FASTENER HOLE, I/B END OF NR 11 SPOILER PNL AND BELOW. REPLACED BRACKET AT I/B END OR NR 11 SPOILER PNL AS PER B77 SRM 51-10-1 PAR 4 AND 51-30-2. N/R 2083.
- [SDR DHL9970234C](https://openairdocs.org/sdr/DHL9970234C.md): Panel · cracked · Jun 23, 1999 · N702DH · Boeing 72730C · Wing, Plate/Skin
  > C CHECK, LW PANEL ON TOP WING HAS I/B SIDE WITH CRACK AND WORN, O/B SIDE OF NR 5 SPOILER. REMOVED CRACKED METAL STRIP ON L/W PANEL O/B OF NR 5 SPOILER PER B727 SRM 51-30-2. REPLACED METAL STRIP ON L/W PANEL O/B OF NR 5 SPOILER PER B727 SRM 51-40-2. TREATED
- [SDR DHL9970229C](https://openairdocs.org/sdr/DHL9970229C.md): Support · cracked · Jun 23, 1999 · N702DH · Boeing 72730C · Wing Miscellaneous Structure
  > C CHECK, RT WING L/E STRUCTURE, CEILING CROSS SUPPORT CRACKED AT O/B END, L/E STA 130.7. REMOVED UNSERVICEABLE CROSS SUPPORT AND REPLACED WITH NEW EXTRUSION ANGLE AS PER B727 CHAP 51-30-2 MAT USED 7075-T6.75 BY3.75 BY X 16 LOT NR 354192 PO NR 831451. ALODIN
- [SDR DHL9970224C](https://openairdocs.org/sdr/DHL9970224C.md): Fitting · corroded · Jun 23, 1999 · N702DH · Boeing 72730C · Leading Edge Devices
  > C-CHECK RT WING L/E FLAP NR 6, MIDDLE HINGE UPPER FITTING SUPPORT (MAGNESIUM) HAS SEVERAL AREAS OF CORROSION OR EROISION (MRKD). REMOVED UPPER HINGE FITTING AND ATTCH LINK FOR INC NR 6 L/E FLAP PER B727 SRM 51-30-2. INSTALLED UPPER HINGE FITTING AT RT L/E FL
- [SDR DHL9970223C](https://openairdocs.org/sdr/DHL9970223C.md): Door · misrepaired · Jun 23, 1999 · N702DH · Boeing 72730C · Cargo/Baggage Doors
  > C CHECK, FWD CARGO COMPARTMENT DOOR, IMPROPER REPAIR DOUBLER INSUFFICIENT AMOUNT OF FASTENERS AND IMPROPERLY COVERING AREA OF DAMAGE. FS 550 AFT BOTTOM SEEN THROUGH THE INSIDE. REMOVED AND REPLACED DAMAGE AREA AT FWD CARGO COMP DOOR AFT BOTTOM INTERIOR OF DO
- [SDR DHL9970222C](https://openairdocs.org/sdr/DHL9970222C.md): Support · cracked · Jun 23, 1999 · N702DH · Boeing 72730C · Wing Miscellaneous Structure
  > C CHECK, RT WING L/E STRUCTURE WBL 92.8 VERT SUPPORT CRACKED AT BOTTOM WITH SEVERAL STOP DRILLED HOLES. CUT OUT DAMAGED SECTON, INSTALLED ANGLE REPAIR 1 BY 1.5 BY 7 PER SRM 51-40-3, N/R 2055.
- [SDR DHL9970210C](https://openairdocs.org/sdr/DHL9970210C.md): Doubler · cracked · Jun 23, 1999 · N702DH · Boeing 72730C · Cargo/Baggage Doors
  > C CHECK, FWD CARGO COMPARTMENT DOOR HAS A CRACKED DOUBLER AT THE AFT BOTTOM INTERIOR OF DOOR. THIS CAN BE SEEN WITH THE DOOR CLOSED AND INSIDE THE CARGO COMPARTMENT AT FS 560. REMOVED AND REPLACED DAMAGE AREA AT FWD CARGO COMP DOOR AFT BOTTOM INTERIOR OF DOOR
- [SDR DHL9970207C](https://openairdocs.org/sdr/DHL9970207C.md): Skin · corroded · Jun 23, 1999 · N702DH · Boeing 72730C · Trailing Edge Flaps
  > C CHECK, LW L/B AFT FLAP HAS CORROSION AND DELAMINATION AT I/B SIDE TOP SKIN. CUT-OUT SMALL CORROSION AND DELAMINATION AREA AND INSTALLED FIBERGLASS OVERLAY REPAIR AT LW I/B AFT FLAP AS PER B727 SRV 51-40-8 FIG 1 MATERIAL USED RES 50-A HARDENER 946 BATCH NR A
- [SDR DHL9970206C](https://openairdocs.org/sdr/DHL9970206C.md): Skin · corroded · Jun 23, 1999 · N702DH · Boeing 72730C · Trailing Edge Flaps
  > C CHECK, LW NR 2 FLAP (1/B) HAS MID FLAP WITH CORROSION AND DELAMINATION ON TOP SKIN ON TOP OF SECOND TRACK FOR AFT FLAP. CUT-OUT SMALL CORROSION AND DELAMINATION AREA AND INSTALLED FIBERGLASS OVERLAY REPAIR AT LW NR 2 FLAP (I/B) MID FLAP PER BOEING 727 SRM 5
- [SDR DHL9970205C](https://openairdocs.org/sdr/DHL9970205C.md): Frame · cracked · Jun 23, 1999 · N702DH · Boeing 72730C · Engine Cowling System
  > C CHECK, NR 2 ENG R4 FWD COWLING FRAME IS CRACKED AT NR 1 GUIDE AREA. CUT OUT DAMAGED SECTION, INSTALLED REPAIR DOUBLER PER SRM 51-40-3, 13 BY 5, N/R 6041.
- [SDR DHL9970201C](https://openairdocs.org/sdr/DHL9970201C.md): Casting · cracked · Jun 23, 1999 · N702DH · Boeing 72730C · Fuselage Miscellaneous Structure
  > C-CHECK, GALLEY DOOR CUTOUT LOWER AFT CORNER CASTING HAS CRACK AND GOUGE. REPLACED CASTING AT DOOR CUT OUT LOWER AFT CORNER IAW B77 SRM 51-30-2, N/R 3121.
- [SDR DHL9970243C](https://openairdocs.org/sdr/DHL9970243C.md): Skin · cracked · Jun 22, 1999 · N702DH · Boeing 72730C · Engine Cowling System
  > C-CHECK, NR 1 ENG INLET COWL CRACKED OUTER SKIN IN POSITION CRACK CONFIRMED BY NDT PART 6-51-00-00 HFEC JRT NDTI58. CUT OUT DAMAGED AREA ON NR 1 ENG NOSE COWL 17 AFT OF L/E AT 12:30 PR B727 SRM 54-30-3, 2.75 BY 8. PERFORMED HFEC INSP PER B7272 HDT MAN PART 6
- [SDR DHL9970238C](https://openairdocs.org/sdr/DHL9970238C.md): Angle · cracked · Jun 22, 1999 · N702DH · Boeing 72730C · Fuselage Miscellaneous Structure
  > C-CHECK, NLG W/W AFT, SUPPORT ANGLE IS CRACKED AT STA 3441, ABOVE LOCK DOWN MECHANISM. REMOVED ANGLE, FOUND WEB CRACKED. CUT OUT DAMAGED AREA OF WEB, HFEC OF AREA. INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 6 BY 7. REPLACED ANGLE PER SRM 51-30-2, 4 BY 12, N
- [SDR DHL9970237C](https://openairdocs.org/sdr/DHL9970237C.md): Skin · damaged · Jun 22, 1999 · N702DH · Boeing 72730C · Fuselage Main, Plate/Skin
  > C-CHECK, AFT UPPER AIRSTAIRS WELL TOP TORQUE BOX SKIN IS OIL CAN BS 1285. CUT OUT DAMAGED AREA AT AFT UPPER AIRSTAIRS WELL, TOP TORQUE BOX SKIN. MAT CUT OUT 18 BY 20 AS PER B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR AT AFT AIRSTAIR TORQUE BOX AREA TOP HORIZ
- [SDR DHL9970236C](https://openairdocs.org/sdr/DHL9970236C.md): Skin · damaged · Jun 22, 1999 · N702DH · Boeing 72730C · Fuselage Main, Plate/Skin
  > C-CHECK, RT UPPER AIRSTAIRS AREA, TOP TORQUE BOX SKIN IS OIL CAN BS 1263 TO 1243. CUT OUT DAMAGED AREA AT RT UPPER AIRSTAIR AREA TOP TORQUE BOX SKIN MAT CUT OUT 15 BY 4 AS PER B727 SRM 51-40-2. INSTALLED DOUBLER REPAIR AT UPPER AIRSTAIR AREA AT RT UPPER SKIN
- [SDR DHL9970233C](https://openairdocs.org/sdr/DHL9970233C.md): Floor · cracked · Jun 22, 1999 · N702DH · Boeing 72730C · Fuselage Floor Panel
  > C CHECK, AFT CARGO COMPARTMENT AFT BULKHEAD AREA BOTTOM OF CABIN FLOOR HAS AREA OF CORROSION AND A CRACK LEFT SIDE. REMOVED FASTENERS AFT CARGO AFT BULKHEAD BOTTOM AREA AS PER 727 SRM 51-30-2. CUT OUT DAMAGE CORRODED AREA AS PER 727 SRM 51-40-2 SIZE CUT OUT
- [SDR DHL9970232C](https://openairdocs.org/sdr/DHL9970232C.md): Seat Track · corroded · Jun 22, 1999 · N702DH · Boeing 72730C · Fuselage, Seat/Cargo Attach Fittings
  > C-CHECK, AFT CARGO COMPT STA 1166 RT SEAT TRACK CRACKED. CUT OUT DAMAGED SECTION FROM STA 1166 TO 1130 AS PER B727 SRM 53-10-5 FIG 8. INSTALLED NEW SECTION OF SEAT TRACK FROM STA 1130 TO STA 1166 AND INSTALLED REPAIR PER B727 SRM 53-10-5 FIG 8 AT STA 1130 MA
- [SDR DHL9970231C](https://openairdocs.org/sdr/DHL9970231C.md): Seat Track · corroded · Jun 22, 1999 · N702DH · Boeing 72730C · Fuselage, Seat/Cargo Attach Fittings
  > C CHECK, AFT CARGO BIN SEAT TRACK CRACKED STA 970 RT SIDE. CUT AND TRIMMED NEW SECTION OF FLOOR TRACK, MADE SPLICE STRIPS, PICKED UP EXISTING FASTENER HOLES AND ADDED NEW ATTACH FASTENER HOLES, TREATED N/R 3096 AND PRIMED ALL NEW AND EXISTING PIECES IAW B727
- [SDR DHL9970227C](https://openairdocs.org/sdr/DHL9970227C.md): Panel · delaminated · Jun 22, 1999 · N702DH · Boeing 72730C · Wing, Plate/Skin
  > C-CHECK, RT WING LOWER SURFACE ACCESS PANEL NR 8505 T/E DELAMINATED (MRK). REMOVED PANEL NR 8505 RT WING LOWER SURFACE FOR FIBERGLASS REPAIR IAW B727-200 12-30-0. INSTALLED BONDING REPAIR AT RT WING LOWER SURFACE ACCESS PANEL NR 8505 T/E AS PER B727 SRM 51-4
- [SDR DHL9970220C](https://openairdocs.org/sdr/DHL9970220C.md): Frame · cracked · Jun 22, 1999 · N702DH · Boeing 72730C · Service Doors
  > C CHECK, RIGHT SERVICE DOOR, THE DOOR FRAME HAS.5 INCH CRACK AREA OF FORWARD NR 2 STOP FROM THE BOTTOM. REMOVED RT SERVICE DOOR IAW B727 MM 52-40-0. INSTALLED RT SERVICE DOOR IAW B727 M/M 52-12-0. ADJUSTED RT SERV DOOR PER B727 M/M 52-12-0. LEAK OK IAW B7
- [SDR DHL9970213C](https://openairdocs.org/sdr/DHL9970213C.md): Skin · cracked · Jun 22, 1999 · N702DH · Boeing 72730C · Spoilers
  > C CHECK, LT/W O/B UPPER T/E PANEL O/B OF NR 1 SPOILER, I/B EDGE OLD REPAIR HAS CRACK AT FASTENER HOLE WS620. REPLACED O/D REPAIR STRAP PR B727 SRM 57-30-4 FIG 10 MATL USED 040 2024T3 APPROX 2 BY 10 LOT NR 44044T25 PMS PO NR 8313480. ALODINED PRIMED TREATED A
- [SDR DHL9970209C](https://openairdocs.org/sdr/DHL9970209C.md): Support · damaged · Jun 22, 1999 · N702DH · Boeing 72730C · Fuselage Miscellaneous Structure
  > C CHECK, FAIRING SUPPORTS AT B5 600 AND 610 ARE BENT AND CRACKED AT LEFT SIDE STRINGER 281. CUT OUT DAMAGED RIB WEB INSTALLED REPAIR PER B727 SRM 51-40-2 AT BS 600 AND BS610 FAIRING SUPPORT MAT USED.040 2024T3 LOT NR 58599511 PMS PO NR 831125 2 PCS APPROX 6

Next page: https://openairdocs.org/deregistered/N702DH-2013-09-20/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 = 'N702DH' AND deregistration_id = 'N702DH-2013-09-20'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N702DH-2013-09-20/reports

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