# Service difficulty reports: N707DH, cancelled May 21, 2015

A list on [N707DH, cancelled May 21, 2015](https://openairdocs.org/deregistered/N707DH-2015-05-21.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 · 121 reports

- [SDR DHL2002707003](https://openairdocs.org/sdr/DHL2002707003.md): Accessory Unit · malfunctioned · Apr 30, 2002 · N707DH · Boeing 72722 · Landing Gear Retraction/Extension System
  > AFTER GEAR RETRACTION MOVED GEAR HANDLE TO OFF, GEAR DOOR LIGHT FORWARD PANEL AND RIGHT MAIN GEAR DOOR LIGHT S/O PANEL ILLUMINATED. MOVED GEAR HANDLE TO UP, LIGHTS OUT, HANDLE TO OFF, LIGHTS OUT NORMAL OPS. ACCOMPLISHED POWER OFF RERACK OF LDG ACCY UNIT, CLE
- [SDR DHL2002707002](https://openairdocs.org/sdr/DHL2002707002.md): Switch · inoperative · Jan 30, 2002 · N707DH · Boeing 72722 · Fire Detection
  > FIRE ALARM BELL DOES NOT WORK FOR ANY ALARM FUNCTION. REMOVED AND REPLACED THE S41 CUTOFF SWITCH WITH SERVICEABLE SWITCH, OPS CHECK GOOD IAW BOEING WM 26-11-01.
- [SDR DHL2002707001](https://openairdocs.org/sdr/DHL2002707001.md): Sensor · failed · Jan 22, 2002 · N707DH · Boeing 72722 · Fire Detection
  > APU FIRE TEST INOP. REMOVED AND REPLACED FIRE DETECTOR SENSOR IAW DHL 727 MM 26-15-002. SYSTEM OPS CHECKED GOOD.
- [SDR DHL2001707015](https://openairdocs.org/sdr/DHL2001707015.md): Autopilot Sys · malfunctioned · Dec 14, 2001 · N707DH · Boeing 72722 · Autopilot System
  > WHILE ON FINAL APPROACH COURSE WITH BOTH LOCALIZERS AND GLIDESLOPE INITIALLY CAPTURED ON AUTOPILOT, THE AUTOPILOT WAS NOT CAPABLE OF FLYING THE GLIDESLOPE. AIRCRAFT DOVE FOR THE GROUND. PERFORMED OPERATIONAL CHECK OF AUTOPILOT SYSTEM IAW 727 MM CH 22-00 AND
- [SDR DHL2001707014](https://openairdocs.org/sdr/DHL2001707014.md): Windshield Wiper · out of adj · Dec 14, 2001 · N707DH · Boeing 72722 · Windshield/Door Rain/Ice Removal
  > RANGE OF MOTION ON WINDSHIELD WIPERS, BOTH CAPT AND F/O ARE INADEQUATE FOR NORMAL FIELD OF VISION (DO NOT COME UP HIGH ENOUGH). WINDSHIELD WIPERS NEED REPLACING (BLADES). TESTED AND ADJUSTED NR 1 AND NR 2 WIPER ASSB IAW 727 MM CHP 30-42. GROUND CKS NORMAL A
- [SDR DHL2001707013](https://openairdocs.org/sdr/DHL2001707013.md): Switch · inoperative · Sep 19, 2001 · N707DH · Boeing 72722 · Landing Gear Position and Warning
  > NOSE GEAR UNSAFE LIGHT DOES NOT ILLUMINATE DURING GEAR RETRACTION OR EXTENSION, LIGHT TEST OK. REMOVED NLG POSITION SWITCH AND LINKAGE PER M/M 32-61-71. INSTALLED NLG POSITION SWITCH IAW B727 MM 32-61-71. OPS CHECK GOOD.
- [SDR DHL2001707012](https://openairdocs.org/sdr/DHL2001707012.md): Battery · discharged · Sep 15, 2001 · N707DH · Boeing 72722 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED BATTERIES IN EMERGENCY EXIT LIGHTS IAW B-M/M 33-50-71.
- [SDR DHL2001707011](https://openairdocs.org/sdr/DHL2001707011.md): Bulkhead · cracked · Sep 1, 2001 · N707DH · Boeing 72722 · Fuselage Main, Bulkhead
  > ON DROP IN CHECK, FWD CARGO COMPT, WING CENTER SECTION FWD BULKHEAD WEB CRACKED (APPROX 1 INCH) RBL 29 APPROX 14 INCHES ABOVE PRESS SPAL BETWEEN VERTICAL ROW OF FASTENERS. STOP DRILLED CRACK 2 PLACES IN FWD CARGO COMPL, WING CENTER SECTION FWD BULKHEAD WEB AT
- [SDR DHL2001707010](https://openairdocs.org/sdr/DHL2001707010.md): Switch · malfunctioned · Aug 4, 2001 · N707DH · Boeing 72722 · Engine Oil Indicating System
  > NR 2 ENGINE OIL PRESSURE LIGHT CAME ON DIM DURING FLIGHT. COULD EXTINGUISH LIGHT BY RETARDING THRUST TO IDLE INITIALLY. BUT EVENTUALLY CAME ON AT IDLE. OIL TEMP READING 135. QUANTITY DECREASED FROM 4.2 GAL AT T/O. R&R MAIN OIL FILTER, FOUND SOME CARBON BB'S NO
- [SDR DHL2001707009](https://openairdocs.org/sdr/DHL2001707009.md): Bleed Valve · failed · Aug 4, 2001 · N707DH · Boeing 72722 · Compressor Bleed Valve
  > T/O THRUST LEFT MANIFOLD DUCT PRESSURE ROSE TO 100PSI DEFERRED PER MAINT. CONTROL 36-11-1 MB. WHEN ATTEMPTING TO START ENGINES TO CHECK PRESSURIZATION, NR 1 ENG WOULD NOT START. NO DUCT PRESSURE DROP AND START VALVE OPEN LIGHT DID NOT ILLUMINATE. RESET C/B-
- [SDR DHL2001707008](https://openairdocs.org/sdr/DHL2001707008.md): Brake · malfunctioned · Jun 21, 2001 · N707DH · Boeing 72722 · Brake Anti-Skid Section
  > AT 38 DEGREES C IN SMF, ANTI-SKID REPEATEDLY RELEASED AS T/O THRUST WAS SET WITH BRAKES ON. FORWARD MOVEMENT OF ACFT WAS MINIMAL. DID NOT OBSERVE RELEASE LIGHTS (DID NOT LOOK). ANTI-SKID NORMAL ON LANDING. ANTI-SKID SYS IS DEFERRED PER MEL32-5, ASSIGNED DMI
- [SDR DHL2001707007](https://openairdocs.org/sdr/DHL2001707007.md): Autopilot Sys · malfunctioned · Jun 8, 2001 · N707DH · Boeing 72722 · Autopilot System
  > WHEN OPERATING AUTOPILOT IN MANUAL MODE USING TURN MODE AUTOPILOT WILL NOT TURN RIGHT. ALL OTHER FUNCTIONS NORMAL. DEFFERED TO DMI 5936, PER MEL 22-1 CAT B, ITEM PLACARD. OPS CHECKED IAW MM 22-11-01, SYSTEM GROUND CHECKS GOOD. PER CREW COMMENT & B727 AUTO-
- [SDR DHL2001707006](https://openairdocs.org/sdr/DHL2001707006.md): Computer · malfunctioned · May 19, 2001 · N707DH · Boeing 72722 · Autopilot Computer
  > WITH AUTOPILOT IN AUTO G/S MODE, AND GLIDE SLOPE CAPTURED, THE AIRCRAFT PITCHES UP AND DOWN AND MAY OR MAY NOT RECOVER TO GLIDE PATH. REPLACED PITCH CHANNEL COMPUTER WITH A SERVICABLE UNIT IAW B727 M/M 22-11-121. CHECKS GOOD AT THIS TIME IAW B727 M/M 22-11-0
- [SDR DHL2001707005](https://openairdocs.org/sdr/DHL2001707005.md): Light · damaged · Apr 10, 2001 · N707DH · Boeing 72722 · Exterior Lighting
  > RIGHT TAIL NAV LIGHT ASSY DAMAGED BY BAGGAGE CART. REPLACED RT WING TIP ASSY IAW MM 57-20-0. STATUS: CLOSED.
- [SDR DHL2001707003](https://openairdocs.org/sdr/DHL2001707003.md): Panel · debonded · Mar 30, 2001 · N707DH · Boeing 72722 · Spoilers
  > UPON ROUTINE A-CHECK INSPECTION, FOUND THE 10 FLIGHT SPOILER PANEL LOWER SKIN SEPARATED FROM PANEL. THE OUTBOARD EDGE WAS COMPLETELY OPEN AND APPEARED THAT SKIN BONDING HAD FAILED. WHEN ATTEMPTING TO MOVE THE PANEL BY HAND, THE PANEL WOULD BUCKLE UNDER PRESS
- [SDR DHL2001707002](https://openairdocs.org/sdr/DHL2001707002.md): Fastener · loose · Feb 12, 2001 · N707DH · Boeing 72722 · Fuselage Main, Structure
  > DURING A/C RECEIVING INSPECTION FOUND LOOSE BLIND FASTENERS ON EXTERNAL SKIN REPAIR BS 218, STRINGER 25R. REMOVED EXTERNAL SKIN REPAIR AND BLIND FASTENERS. INSTALLED EXTERNAL REPAIR WITH SOLID FASTENERS AT BS 218, STRINGER 25R IAW B727 SRM 53-30-3.
- [SDR DHL2001707001](https://openairdocs.org/sdr/DHL2001707001.md): Motor · inoperative · Feb 7, 2001 · N707DH · Boeing 72722 · Windshield/Door Rain/Ice Removal
  > CAPTS WINDSHIELD WIPERS INOP IN ALL SPEEDS. REMOVED AND REPLACED CAPTS WIPER MOTOR IAW MM 30-42-11.
- [SDR DHL2000707037](https://openairdocs.org/sdr/DHL2000707037.md): Skin · damaged · Sep 19, 2000 · N707DH · Boeing 72722 · Fuselage Main, Plate/Skin
  > HOLE IN FUSELAGE, FWD RT SIDE OF NOSE, AFT OF RADOME. REPAIR SKIN USING PROCEDURES OUTLINED IN THE SRM 53-30-3 PG 74C -- 74F. THIS IS AN INTERM REPAIR.
- [SDR DHL2000707031](https://openairdocs.org/sdr/DHL2000707031.md): Turbine · failed · Aug 31, 2000 · N707DH · Boeing 72722 · Turbine Section
  > NR 3 ENGINE FAILED ON T/O, ENGINE SHUT DOWN (POWER LOSS). EMERGENCY DECLARED, RETURNED TO BWI. INITIAL INSPECTION INDICATES TURBINE FAILURE.
- [SDR DHL2000707032](https://openairdocs.org/sdr/DHL2000707032.md): Engine · failed · Aug 31, 2000 · N707DH · Boeing 72722 · Engine (Turbine/Turboprop)
  > NR 3 ENG FAILED ON L/O. ENGINE SHUT DOWN, EMERGENCY WAS DECLARED AND RETURN TO BWI. A/C WAS FERRIED TO CVG FOR ENG CHANGE. REMOVED AND REPLACED NR 3 ENGINE.
- [SDR DHL2000707030](https://openairdocs.org/sdr/DHL2000707030.md): Indicator · failed · Jul 7, 2000 · N707DH · Boeing 72722 · Airspeed/Mach Indicator
  > REJECTED TAKE OFF, NO AIRSPEED INDICATION ON CAPTAIN SIDE.VERIFIED NO OBSTRUCTION IN CAPT PITOT.REMOVED AND REPLACED MACH AIR SPEED INDR.AND OPS CHKD IAW MM 34-11-10 AND 34-11-40.
- [SDR DHL2000707029](https://openairdocs.org/sdr/DHL2000707029.md): Warning Light · illuminated · Jul 7, 2000 · N707DH · Boeing 72722 · Brake Anti-Skid Section
  > ON TACK OFF ROLL THE RIGHT INBD MAIN LANDING GEAR ANTI-SKID LIGHT ILLUMINATED AT 60 KTS,REJECTED TAKE OFF. PLACED ON D M I PER MEL 32-05.
- [SDR DHL200070729C](https://openairdocs.org/sdr/DHL200070729C.md): Panel · chipped · Jun 8, 2000 · N707DH · Boeing 72722 · Vertical Stabilizer, Plate/Skin
  > AT C CK; RT VERTICAL STAB PANEL 9604-HONEYCOMB SHOWING THRU AND CHIPPED SURFACE. INSTALLED FIBERGLASS CLOTH OVERLAY REPAIR PER B727 SRM 51-40-8 FIG. 1. PAINTED RH VERT STAB IAW B727 M/M 51-20-0. REF: N/R 4543.
- [SDR DHL200070728C](https://openairdocs.org/sdr/DHL200070728C.md): Skin · delaminated · Jun 8, 2000 · N707DH · Boeing 72722 · Aerodynamic Fairings
  > AT C CK; AFT CARGO DOOR MOVABLE FAIRING EXTERNAL SKIN HAS DELAMINATION ON DIFFERENT PLACES. INSTALLED FIBERGLASS OVERLAY REPAIR AFT CARGO DOOR FAIRING EXTERNAL SKIN PER B727 SRM 51-40-8 FIG. 1, PAINTED AS REQUIRED IAW B727 M/M 51-20-0. REF: N/R 3347.
- [SDR DHL200070726C](https://openairdocs.org/sdr/DHL200070726C.md): Support Bracket · cracked · Jun 1, 2000 · N707DH · Boeing 72722 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY, LT SIDE WALL SUPPORT, CRACKED STA 540 ABOVE STR 26 LT. REMOVED DAMAGED SECTION OF SIDE WALL LINER SUPPORT FROM STA 480 TO STA 530 ABOVE STR 26 LT. REPLACED SIDE WALL SUPPORT STA 480 STR 26L TO STA 530 STR 26 LT. TREATED AND PRIMED SIDE WALL SUP
- [SDR DHL200070733C](https://openairdocs.org/sdr/DHL200070733C.md): Tab · delaminated · May 26, 2000 · N707DH · Boeing 72722 · Rudder, Tab Structure
  > AT C CK; LWR RUDDER TAB LWR LT & RT SURFACE DELAMINATED. ACCOMPLISHED FIBERGLASS CLOTH OVERLAY REPAIR PER B727 SRM 51-40-8 FIG 1. REF: N/R 4545.
- [SDR DHL200070730C](https://openairdocs.org/sdr/DHL200070730C.md): Cowling · worn · May 26, 2000 · N707DH · Boeing 72722 · Engine Cowling System
  > AT C CK; NR 2 ENGINE RT/AFT COWLING WORN AT LOWER SIDE OF NR 7 RIB. CUTOUT WORN AREA AT NR 2 ENGINE RT AFT COWLING AT RIB NR 7, 6 INCH X 1&1/8 INCH PER B727 SRM 51-30-2, FABRICATED AND INSTALLED DOUBLER REPAIR PER B727 SRM 54-10-3. REF: N/R 6142.
- [SDR DHL200070704C](https://openairdocs.org/sdr/DHL200070704C.md): Fitting · cracked · May 24, 2000 · N707DH · Boeing 72722 · Fuselage Miscellaneous Structure
  > FS 870 RT TERMINAL FITTING AT SPLICE FWD BETWEEN STR 9 & 10 SHOWS CRACK. REMOVED FASTENERS FWD OF SPLICE STA 870 RT STR 9 & 10. REMOVED FWD SPLICE FOR INSP SRM 51-30-2. FWD SPLICE AT 870 RT FWD SIDE CRACK COMING FROM LOWER HOLE FWD ROW OF SPLICE. ACCOMP HF
- [SDR DHL200070725C](https://openairdocs.org/sdr/DHL200070725C.md): Lap Joint · damaged · May 23, 2000 · N707DH · Boeing 72722 · Fuselage Main, Plate/Skin
  > 1080 LAP JOINT HAS + 10 PERCENT INDICATION OF CORROSION BELOW S-2 LT, FROM LBL 13 TO 14 AFT OF AFT FASTNER ROW. REMOVED FASTENERS AND CUT OUT DAMAGED AREA OF AFT SKIN BS 1080 FROM STR 4 LT TO 4 RT, 1/4 IN X 4 1/8 IN. VISUAL INSPECTION FROM S 10 LT TO S 10 RT
- [SDR DHL200070711C](https://openairdocs.org/sdr/DHL200070711C.md): Angle · broken · May 23, 2000 · N707DH · Boeing 72722 · Fuselage Miscellaneous Structure
  > NR 2 ENGINE FWD MOUNTS REAR AREA BS 1400 APROX METAL ANGLE STRIP BROKEN. REMOVED AND REPLACED ANGLE STRIP PER SRM 51-30-2. TREATED AND PRIMED PER SRM 51-10-2.
- [SDR DHL200070708C](https://openairdocs.org/sdr/DHL200070708C.md): Skin · corroded · May 23, 2000 · N707DH · Boeing 72722 · Fuselage Main, Plate/Skin
  > 1080 CIR JOINT HAS + 10 PERCENT CORROSION LOSS IND FROM LBL 7 AFT OF FASTENER ROW. REMOVED FASTENERS AND CUT OUT DAMAGED SECTION OF AFT SKIN BS 1080 FROM STR 4L TO STR 4R 59.25 X 4.125 PER S/B 727-53-0109. VISUAL INSP COMPLEATED FROM STA 102 TO 10R, NO FURTH
- [SDR DHL200070732C](https://openairdocs.org/sdr/DHL200070732C.md): Skin · cracked · May 20, 2000 · N707DH · Boeing 72722 · Service Doors
  > AT C CK; CABIN SERVICE DOOR HAS CRACK ON EXTERNAL SKIN ON UPPER HINGE AREA. STOP DRILLED CRACK PER B727 SRM 51-10-1, PERFORMED HFEC PER NDT M/M 51-00-00 PART 6 FIG 4, NO CRACK INDICATIONS NOTED, INSTALLED DOUBLER REPAIR PER B727 SRM 51-40-2. (SIZE OF REPAIR-3
- [SDR DHL200070720C](https://openairdocs.org/sdr/DHL200070720C.md): Doubler · cracked · May 20, 2000 · N707DH · Boeing 72722 · Wing Miscellaneous Structure
  > CORRUGATED DOUBLER CRACKED AT T/E AREA L/W SPAR LOWER SECTION APPROX WS 546.5 (I/B SECTION OF STATION). STOP DRILLED CRACK AT CORRUGATED STRAP AT FT WING REAR SPAR AT WS 546.5 PER SRM 51-10-1. PERFORMED HFEC INSP PER NDT MAN PART 6-51-00-00 FIG 4. NO CRACK
- [SDR DHL200070715C](https://openairdocs.org/sdr/DHL200070715C.md): Skin · cracked · May 19, 2000 · N707DH · Boeing 72722 · Passenger/Crew Doors
  > CABIN SERVICE DOOR HAS CRACK ON EXTERNAL SKIN ON UPPER HINGE PANEL. STOP DRILLED CRACK AT CABIN SERVICE DOOR ON UPPER HINGE AREA PER SRM 51-10-1.PERFORMED HFEC INSP PER NDT MAN 51-00-00 FIG 4, NO CRACK INDICATION NOTED. INSTALLED DOUBLER REPAIR AT CABIN SERV
- [SDR DHL200070724C](https://openairdocs.org/sdr/DHL200070724C.md): Plate · cracked · May 18, 2000 · N707DH · Boeing 72722 · Fuselage Miscellaneous Structure
  > MAIN CARGO DOOR CUT OUT SCUFF PLATE AND ADJACENT COVER WORN AND CRACKED AT FWD LOWER CORNER. SMOOTHED OUT SCUFF PLATE AT CARGO DOOR, FWD LOWER CUT OUT AS PER SRM 51-10-1. MATERIAL LOST.003 INCH, WITHIN LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED COVER PER S
- [SDR DHL200070723C](https://openairdocs.org/sdr/DHL200070723C.md): Skin · cracked · May 18, 2000 · N707DH · Boeing 72722 · Horizontal Stabilizer, Plate/Skin
  > LT HORIZ STAB L/E SKIN HAS A CRACK AT RIVET HEAD STA 47.3. PERFORMED HFEC INSP AND CONFIRMED CRACK PER NDT MAN 51-00-00 PART 6 FIG 4. CUT OUT DAMAGED AREA 2.5 X 1.75 INCH PER SRM 55-10-3. APPLIED ALODINE AND PRIMER PER SRM 51-10-2. INSTALLED REPAIR AT LT H
- [SDR DHL200070707C](https://openairdocs.org/sdr/DHL200070707C.md): Frame · cracked · May 18, 2000 · N707DH · Boeing 72722 · Landing Gear Doors
  > RT MAIN LANDING GEAR WING DOOR LOWER END FRAME IS CRACKED ON O/B BEND RADIUS AT FWD END. REMOVED CRACKED END FRAME AT RT MLG WING DOOR LWR END AS PER SRM 51-30-2. INSTALLED NEW END FRAME AT RT MLG WING DOOR LOWER END FWD SIDE PER SRM 51-30-2. TREATED AND PR
- [SDR DHL200070706C](https://openairdocs.org/sdr/DHL200070706C.md): Skin · corroded · May 18, 2000 · N707DH · Boeing 72722 · Fuselage Main, Plate/Skin
  > 1808 CR JOINT HAS +10 PERCENT IND OF CORROSION BELOW S 2L FROM LBL 13 TO 14 AFT OF AFT FASTENER ROW. REMOVED FASTENERS AND CUT OUT DAMAGED SECTION OF SKIN BS 1080 FROM STR 4L TO 4R AS PER S/B 727-53-0109. VISUAL INSP ACCOMPLISHED, NO FURTHER CORROSION NOTED.
- [SDR DHL200070703C](https://openairdocs.org/sdr/DHL200070703C.md): Skin · corroded · May 18, 2000 · N707DH · Boeing 72722 · Fuselage Main, Plate/Skin
  > 1080 CIR JOINT HAS 2090 CORR LOSS FROM S-8R TO S10R AFT OF AFT FASTENER ROW. REMOVED FASTNERS AND CUT OUT DAMAGED SECTION OF AFT SKIN 13S 1080 FROM STR 10R TO STR 4R 59.375 X 4.125 AS PER S/B 53-0109 R 4. VISUAL INSP ACCOMP FROM 10L STRINGER TO 10R STRINGER
- [SDR DHL200070719C](https://openairdocs.org/sdr/DHL200070719C.md): Panel · cracked · May 17, 2000 · N707DH · Boeing 72722 · Leading Edge Devices
  > NR 6 L/E SLAT ANTI-ICE TELOSCOPIC DUCT FAIRING PANEL CRACKED. REMOVED AND REPLACED ANTI ICE DUCT PANEL ON NR 6 L/E SLAT PER SRM 51-30-2. ALODINED AND PRIMED PER SRM 51-10-2.
- [SDR DHL200070718C](https://openairdocs.org/sdr/DHL200070718C.md): Skin · scratched · May 17, 2000 · N707DH · Boeing 72722 · Wing, Plate/Skin
  > RT WING UPPER SKIN HAS DEEP SCRATCH AT WS 546.5 APPROX. CUT OUT DAMAGED AREA AT L/E RT WING UPPER SKIN AS PER 727 SRM 57-30-4 FIG 2, CUT DIMENSIONS 4 X 2 IN. INSTALLED FLUSH REPAIR AT RT WING L/E AS PER SRM 57-30-4 FIG 2. ALODINED AND PRIMED AS PER SRM 51-1
- [SDR DHL200070716C](https://openairdocs.org/sdr/DHL200070716C.md): Angle · chafed · May 17, 2000 · N707DH · Boeing 72722 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT FLOORBEAM SUPPORT ANGLE IS WORN (CHAFED) ON TOP BS 111073 ABOVE STR 29R. CUT OUT DAMAGED AREA AT CARGO SUPPORT ANGLE AT AFT CARGO COMPT SUPPORT ANGLE AT BS 1110 STR 29R. CUT OUT SIZE 3 X 1 IN AS PER SRM 51-40-3. INSTALLED ANGLE REPAIR AT CAR
- [SDR DHL200070710C](https://openairdocs.org/sdr/DHL200070710C.md): Rib · cracked · May 17, 2000 · N707DH · Boeing 72722 · Aerodynamic Fairings
  > TAIL CONE INTERIOR RIB CROSS SUPPORT ANGLE CRACKED. REMOVED FIBERGLASS RIB CROSS SUPPORT ANGLE AT TAIL CONE PER SRM 51-30-2. APPLIED FIBERGLASS CLOTH OVERLAY REPIAR TO INTERIOR RIB CROSS SUPPORT ANGLE PER SRM 51-40-8 FIG 1. INSTALLED RIB SUPPORT ANGLE PER S
- [SDR DHL200070702C](https://openairdocs.org/sdr/DHL200070702C.md): Rivet · loose · May 17, 2000 · N707DH · Boeing 72722 · Engine Cowling System
  > NR 1 ENG, LWR COWLING SHOWS 8 WORKING RIVETS AT LOWER MID AREA. CUT OUT DAMAGED AREA 13.5 IN X 2.5 IN PER SRM 54-10-3 FIG 5. CLEANED, ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED REPAIR PARTS PER SRM 54-10-3 FIG 5.
- [SDR DHL200070721C](https://openairdocs.org/sdr/DHL200070721C.md): Slat Track · cracked · May 16, 2000 · N707DH · Boeing 72722 · Leading Edge Devices
  > THE NR 2 SLAT O/B TRACK TO SLAT ATTACH CLIP IS CRACKED ON THE I/B RADIUS. REPLACED ATTACH CLIP AT NR 2 SLAT O/B TRACK TO SLAT PER SRM 51-30-2.
- [SDR DHL200070709C](https://openairdocs.org/sdr/DHL200070709C.md): Angle · cracked · May 16, 2000 · N707DH · Boeing 72722 · Fuselage Miscellaneous Structure
  > LEFT W/W, VERT ANGLE BETWEEN BULKHEAD 870 AND KEEL BEAM HAS CRACK, FWD SIDE OF APU. VERIFIED CRACK PER NDT M/M PART 6-51-00 FIG 4. REMOVED VERT ANGLE PER SRM 51-30-2. INSTALLED NEW VERT ANGLE AT LEFT W/W PER SRM 53-10-2. ALODINED AND PRIMED PER SRM 51-10-2
- [SDR DHL200070727C](https://openairdocs.org/sdr/DHL200070727C.md): Skin · delaminated · May 15, 2000 · N707DH · Boeing 72722 · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STAB, ELEVATOR UPPER SURFACE, HAS SEVERAL AREAS DELAMINATED. OPENED ACCESS PANEL FOR EVALUATION. REMOVED LT HORIZONTAL STAB ELEVATER UPPER SKIN FROM STA 151.81 TO STA 188.65. INSTALLED PANEL SKIN.INSTALLED BALANCE PANEL SEALED PANEL REBALANCED EL
- [SDR DHL200070713C](https://openairdocs.org/sdr/DHL200070713C.md): Seat Track · worn · May 15, 2000 · N707DH · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 24 HAS LOCK LUG WORN STA 850. REMOVED SEAT TRACK PER SRM 51-30-2. INSTALLED NEW SEAT TRACK FROM STA 850 TO 870 PER SRM 53-10-5. ALODINED AND PRIMED PER SRM 51-10-2.
- [SDR DHL200070712C](https://openairdocs.org/sdr/DHL200070712C.md): Seat Track · worn · May 15, 2000 · N707DH · Boeing 72722 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 45 HAS LOCK LUG WORN AT STA 860. REMOVED SEAT TRACK AT BS 860 LBL 45 PER SRM 51-30-2. INSTALLED SEAT TRACK SECTION PER M/M 53-4-0 AND SRM 51030-2. MATERIAL USED SEAT TRACK 91 IN 1778 T6 511. ALODINED AND PRIMED PER SRM 51-10-2.
- [SDR DHL200070722C](https://openairdocs.org/sdr/DHL200070722C.md): Fairing · torn · May 13, 2000 · N707DH · Boeing 72722 · Wing Miscellaneous Structure
  > NR 7 FLAP JACKSCREW FAIRING TORN AT I/B EDGE, UPPER SURFACE. CUT OUT DAMAGED AREA AT NR 7 JACKSCREW FAIRING I/B EDGE PER SRM 51-40-2. MATRL LOSS.5 INCH. INSTALLED EXTERNAL DOUBLER PER SRM 51-4-02 FIG 1. ALODINED AND PRIMED AREA PER 51-10-2.

Next page: https://openairdocs.org/deregistered/N707DH-2015-05-21/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 = 'N707DH' AND deregistration_id = 'N707DH-2015-05-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N707DH-2015-05-21/reports

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